Apparatus for manufacture of at least two solar cell arrangements, system for manufacture of at least two shingled solar cells, and method for manufacture of at least two solar cell arrangements

ABSTRACT

The present disclosure provides a support device for conveying at least one solar cell element in a transport direction, wherein the support device comprises a support element configured for supporting the at least one solar cell element and an electric arrangement configured for providing an electrostatic force for holding the at least one solar cell element on the support element.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation application of U.S. patentapplication Ser. No. 15/326,711, filed as application No.PCT/EP2016/060196, on May 6, 2016.

FIELD

Embodiments of the present disclosure relate to an apparatus formanufacture of at least two solar cell arrangements, a system formanufacture of at least two shingled solar cells, and a method formanufacture of at least two solar cell arrangements. Embodiments of thepresent disclosure particularly relate to an apparatus, system andmethod for manufacture of shingled solar cells.

BACKGROUND

Solar cells are photovoltaic devices that convert sunlight directly intoelectrical power. An efficiency of the solar cells can be affected by anactive area on a front surface of the solar cell that is exposed tolight for converting sunlight into electrical power. The active area canbe reduced due to the presence of electrical contacts, such as fingersand/or busbars, on the front surface of the solar cells. The presence ofthe electrical contacts on the front surface of the solar cells can thusreduce a module power of a solar cell module consisting of the solarcells.

In view of the above, new apparatuses and methods for manufacture of atleast two solar cell arrangements and systems for manufacture of atleast two shingled solar cells, that overcome at least some of theproblems in the art are beneficial. The present disclosure particularlyaims at providing solar cell arrangements that have an increasedefficiency and that can be easily produced. Embodiments moreparticularly aim at solar cell arrangements, e.g., of solar cellmodules, that allow to increase a module power.

SUMMARY

In light of the above, an apparatus for manufacture of at least twosolar cell arrangements, a system for manufacture of at least twoshingled solar cells, and a method for manufacture of at least two solarcell arrangements are provided. Further aspects, benefits, and featuresof the present disclosure are apparent from the claims, the description,and the accompanying drawings.

According to an aspect of the present disclosure, an apparatus formanufacture of at least two solar cell arrangements is provided. Theapparatus includes a separation device configured for separating a firstsolar cell into two or more first solar cell pieces, and at least onepositioning device configured for positioning at least one first solarcell piece of the two or more first solar cell pieces on a supportdevice for forming a first solar cell arrangement of the at least twosolar cell arrangements and for positioning at least one other firstsolar cell piece of the two or more first solar cell pieces on thesupport device for forming a second solar cell arrangement of the atleast two solar cell arrangements.

According to another aspect of the present disclosure, a system formanufacture of at least two shingled solar cells is provided. The systemincludes the apparatus for manufacture of at least two solar cellarrangements according to the embodiments described herein, and aproduction tool for manufacturing a plurality of solar cells includingthe first solar cell, wherein the plurality of solar cells are inputinto the apparatus.

According to a further aspect of the present disclosure, a method formanufacture of at least two solar cell arrangements is provided. Themethod includes a separating of each solar cell of one or more solarcells into two or more solar cell pieces, and a forming at least a firstsolar cell arrangement and a second solar cell arrangement of the atleast two solar cell arrangements from the two or more solar cellpieces, wherein each solar cell piece of the two or more solar cellpieces is allocated to the first solar cell arrangement or the secondsolar cell arrangement based on one or more geometric and/or physicalproperties of the solar cell piece.

According to an aspect of the present disclosure, a support device forconveying at least one solar cell element in a transport direction isprovided. The support device includes a support element configured forsupporting the at least one solar cell element and an electricarrangement configured for providing an electrostatic force for holdingthe at least one solar cell element on the support element.

According to yet another aspect of the present disclosure, a method forconveying at least one solar cell element in a transport direction isprovided. The method includes providing an electric charge to a supportelement configured for supporting at least one solar cell element,holding the at least one solar element by an electrostatic force, andmoving the at least one solar element in the transport direction.

Embodiments are also directed at apparatuses for carrying out thedisclosed methods and include apparatus parts for performing eachdescribed method aspect. These method aspects may be performed by way ofhardware components, a computer programmed by appropriate software, byany combination of the two or in any other manner. Furthermore,embodiments according to the disclosure are also directed at methods foroperating the described apparatus. The methods for operating thedescribed apparatus include method aspects for carrying out everyfunction of the apparatus.

BRIEF DESCRIPTION OF THE DRAWINGS

So that the manner in which the above recited features of the presentdisclosure can be understood in detail, a more particular description ofthe disclosure, briefly summarized above, may be had by reference toembodiments. The accompanying drawings relate to embodiments of thedisclosure and are described in the following:

FIG. 1 shows a schematic view of an apparatus for manufacture of atleast two solar cell arrangements according to embodiments describedherein;

FIG. 2 shows a schematic views of a shingled solar cell manufacturedusing the apparatuses, systems and methods according to the embodimentsdescribed herein;

FIGS. 3A to C show schematic views of a separation device according toembodiments described herein;

FIG. 4A shows a schematic side view of an apparatus for manufacture ofat least two solar cell arrangements according to further embodimentsdescribed herein;

FIG. 4B shows a schematic top view of an apparatus for manufacture of atleast two solar cell arrangements according to yet further embodimentsdescribed herein;

FIG. 5 shows a schematic view of overlapping solar cell pieces on asupport device according to embodiments described herein;

FIGS. 6A and B show schematic views of a positioning device according toembodiments described herein;

FIGS. 7A and B show schematic views of a full-square solar cell and apseudo-square solar cell, respectively, according to embodimentsdescribed herein;

FIG. 8A shows a schematic view of an apparatus for manufacture of atleast two solar cell arrangements according to embodiments describedherein;

FIG. 8B shows a schematic view of an apparatus for manufacture of atleast two solar cell arrangements according to further embodimentsdescribed herein;

FIG. 8C shows a schematic view of an apparatus for manufacture of atleast two solar cell arrangements according to yet further embodimentsdescribed herein;

FIG. 9A shows a schematic view of a system for manufacture of a at leasttwo shingled solar cells according to embodiments described herein;

FIG. 9B shows a schematic view of a system for manufacture of at leasttwo shingled solar cells according to further embodiments describedherein;

FIG. 10 shows a flow chart of a method for manufacture of at least twosolar cell arrangements according to embodiments described herein;

FIG. 11 shows a schematic side view of an electrostatic support deviceaccording to embodiments described herein;

FIG. 12 shows a schematic perspective view of an electrostatic supportdevice according to further embodiments described herein;

FIG. 13 shows a schematic view of a part of an electric arrangement forproviding an electrical charge to the electrostatic support deviceaccording to some embodiments described herein;

FIG. 14A shows a schematic top view of a flexible panel of theelectrostatic support device according to embodiments described herein;

FIG. 14B shows a schematic back view of a flexible panel of theelectrostatic support device according to embodiments described herein;

FIG. 15 shows a cross-sectional view of a layer structure of a flexiblepanel of the electrostatic support device according to embodimentsdescribed herein;

FIG. 16 shows a schematic view of an electrostatic support device havinga multi-control configuration according to some embodiments describedherein; and

FIG. 17 shows a schematic view of an electrostatic support device havinga multi-control configuration according to some further embodimentsdescribed herein.

DETAILED DESCRIPTION OF EMBODIMENTS

Reference will now be made in detail to the various embodiments of thedisclosure, one or more examples of which are illustrated in thefigures. Within the following description of the drawings, the samereference numbers refer to same components. Generally, only thedifferences with respect to individual embodiments are described. Eachexample is provided by way of explanation of the disclosure and is notmeant as a limitation of the disclosure. Further, features illustratedor described as part of one embodiment can be used on or in conjunctionwith other embodiments to yield yet a further embodiment. It is intendedthat the description includes such modifications and variations.

The solar cell arrangements of the present disclosure can be shingledsolar cells, which can also be referred to as “hypercells” or“supercells”. The solar cell arrangements, can be used in solar cellmodules. The solar cell arrangements can be made of a plurality ofpartially overlapping solar cell pieces (also referred to as “solar cellelements”). Adjacent solar cell pieces are electrically connected toeach other in the overlapping region. The solar cell pieces areconnected in series such that current generated by the individual solarcell pieces flows along the series of solar cell pieces to be collected,for example, at an end portion of the solar cell arrangement. Theoverlapping configuration can provide high-efficiency solar cellarrangements. In particular, the solar cell arrangements allow toincrease a module power by increasing a used or active area. Typically,the overlapping configuration can increase the module power by, forexample, 20 to 40 Watts. The used or active area can correspond to anarea that is irradiated by solar light and that participates in thegeneration of power. As an example, the used or active area cancorrespond to an area of the solar cells that is not covered by, forexample, conductive line patterns, such as fingers and/or busbars.

In some cases, a solar cell piece of a solar cell arrangement can have ahigh resistance and/or low efficiency when compared to the other solarcell pieces of the solar cell arrangement. An overall performanceincluding, but not limited to, the module power of the solar cellarrangement and/or solar cell module can be affected or determined to aconsiderable extent by the solar cell piece having the high resistanceand/or low efficiency. This low-quality solar cell piece particularlyacts as a “bottleneck” within the solar cell arrangement.

The embodiments of the present disclosure separate, e.g., cleave a solarcell into smaller pieces, which are then sorted and allocated to atleast two different solar cell arrangements. As an example, each solarcell piece can be allocated to a respective solar cell arrangement basedon one or more geometric and/or physical properties of the solar cellpiece. A solar cell arrangement can thus be made of solar cell elementshaving similar characteristics and/or quality, and an overall efficiencyof the solar cell arrangement can be improved. A module power of thesolar cell module having the solar cell arrangement can be increased,particularly since “bottlenecks” due to low-quality solar cell piecescan be avoided.

FIG. 1 shows a schematic view of an apparatus 100 for manufacture of atleast two solar cell arrangements according to embodiments describedherein. The apparatus 100 can be part of a larger production line, as itis for example described with respect to FIGS. 8 and 9 .

The apparatus 100 includes a separation device 110 configured forseparating a solar cell 10, such a first solar cell, into two or morefirst solar cell pieces, and at least one positioning device 120configured for positioning at least one first solar cell piece 11 of thetwo or more first solar cell pieces on a support device 130 for forminga first solar cell arrangement of the at least two solar cellarrangements and for positioning at least one further or other firstsolar cell piece 12 of the two or more first solar cell pieces on thesupport device 130 for forming a second solar cell arrangement of the atleast two solar cell arrangements. The solar cell pieces, such as thetwo or more first solar cell pieces, can also be referred to as “solarcell elements” or “small(er) cells”.

The apparatus 100 divides the solar cell 10 into a plurality of solarcell pieces, wherein at least two solar cell pieces of said solar cell10 are allocated to two different solar cell arrangements. As anexample, the solar cell arrangements can be shingled solar cells,wherein solar cell pieces of one or more solar cells including the firstsolar cell can be allocated to the respective solar cell arrangementbased on characteristics and/or quality of the individual solar cellsand/or solar cell pieces. An efficiency of the solar cell arrangementcan be improved, particularly since “bottlenecks” in the solar cellarrangement due to low-quality and/or high-resistance pieces can beavoided.

According to some embodiments, which can be combined with otherembodiments described herein, the apparatus 100 further includes acentering device, such as a mechanical centering device, configured tocenter or align the solar cell 10 which is to be divided into the two ormore solar cell pieces. As an example, the centering device can beprovided at the separation device 110 to center or align the solar cell10 with respect to the separation device 110. In particular, the solarcell 10 can be centered or aligned before the solar cell 10 is inputtedinto the separation device 110.

In some implementations, the solar cell 10 which is divided into the twoor more solar cell pieces, such as the two more first pieces, can haveone or more conductive patterns, such as fingers and/or busbars,provided thereon. In particular, the term “solar cell” can refer to afinished or nearly finished solar cell instead of, for example, anunprocessed semiconductor substrate. The solar cell 10 can have afrontside and a backside. Fingers and/or busbars can be deposited on thefrontside, for example, using a printing technique such as screenprinting. Optionally, the solar cell 10 can have one or more backsidecontacts.

According to some embodiments, which can be combined with otherembodiments described herein, the at least one positioning device 120 isconfigured to arrange a plurality of solar cell pieces, such as aplurality of first solar cell arrangement pieces, including the at leastone first solar cell piece 11 on the support device 130 with adjacentsolar cell pieces partly overlapping with each other to form the firstsolar cell arrangement. The at least one positioning device 120 can befurther configured to arrange a plurality of other solar cell pieces,such as a plurality of second solar cell arrangement pieces, includingthe at least one other first solar cell piece 12 on the support device130 with adjacent solar cell pieces partly overlapping with each otherto form the second solar cell arrangement. Accordingly, the hypercellcan be formed by smaller cells assembled as shingles. The overlappingconfiguration of a solar cell arrangement is further explained withrespect to FIG. 2 .

According to some embodiments, the separation device 110 is configuredfor separating a second solar cell into two or more second solar cellpieces. The first solar cell and the second solar cell can be inputtedinto and/or processed by the separation device 110 sequentially orsimultaneously. In particular, the separation device 110 can beconfigured for sequentially or simultaneously separating the first solarcell and the second solar cell into the two or more first solar cellpieces and the two or more second solar cell pieces, respectively. Thepositioning device 120 can be configured for positioning at least onesecond solar cell piece of the one or more second solar cell pieces onthe support device 130 for forming the first solar cell arrangementtogether with the at least one first solar cell piece 11, and can beconfigured for positioning at least one other second solar cell piece ofthe two or more second solar cell pieces on the support device 130 forforming the second solar cell arrangement together with the at least oneother first solar cell piece 12.

In particular, a plurality of solar cells can be divided into solar cellpieces, wherein each solar cell piece is allocated to either the firstsolar cell arrangement or the second solar cell arrangement. The solarcell pieces of the first solar cell arrangement can particularly includethe at least one first solar cell piece 11 and the at least one secondsolar cell piece, and can optionally further include one or more solarcell pieces of further solar cells, such as a third, fourth, and so onsolar cell. The solar cell pieces, e.g., of the second solar cellarrangement can include the at least one other first solar cell piece 12and the at least one other second solar cell piece, and can optionallyfurther include one or more solar cell pieces, e.g., of further solarcells, such as the third, fourth, etc solar cell.

In some implementations, the apparatus 100 is configured to allocateeach solar cell piece, such as the solar cell pieces of the two or morefirst solar cell pieces, to either the first solar cell arrangement orthe second solar cell arrangement based on one or more properties (e.g.,geometric and/or physical properties) of the respective solar cellpiece. As an example, each solar cell piece of the plurality of solarcells can be allocated to either the first solar cell arrangement or thesecond solar cell arrangement, for example, based on one or morecharacteristics or properties of the respective solar cell piece. Theone or more characteristics or properties of the solar cell piece may beselected from the group consisting of geometric shape, electricalproperties, optical properties, printing quality, and any combinationthereof.

In some implementations, the at least two solar cell arrangements, suchas the first solar cell arrangement and the second solar cellarrangement, can be arranged in parallel on the support device 130, forexample, along a transport direction provided by the support device 130.In particular, the at least two solar cell arrangements, such as thefirst solar cell arrangement and the second solar cell arrangement, canbe assembled simultaneously by dividing the plurality of solar cellsinto solar cell pieces and selectively allocating the solar cell piecesto the first solar cell arrangement and the second solar cellarrangement.

Although the example of FIG. 1 shows two solar cell arrangements on thesupport device 130 that are assembled in parallel, it is to beunderstood that the present disclosure is not limited thereto and thatany number of solar cell arrangements could be assembled in parallel. Asan example, the at least two solar cell arrangements can be two, three,four five, or even six solar cell arrangements, including the firstsolar cell arrangement and the second solar cell arrangement, that canbe assembled in parallel. At least some of the solar cell arrangementscan have different characteristics or quality based on the properties ofthe solar cell pieces which have been allocated to the individual solarcell arrangement.

According to some embodiments, which can be combined with otherembodiments described herein, a solar cell arrangement, such as ashingled solar cell, can include two or more solar cell pieces.

FIG. 2 shows a schematic view of a solar cell arrangement 20, which is ashingled solar cell or hypercell, and that can be manufactured using theapparatuses, systems and methods according to the embodiments describedherein. The solar cell arrangement 20 can be used in a solar cellmodule, which is a packaged, connected assembly of a plurality of solarcells or solar cell arrangements.

The shingled solar cell includes a plurality of overlapping solar cellpieces, such as the plurality of first solar cell arrangement pieces orthe plurality of second solar cell arrangement pieces described withrespect to FIG. 1 . As an example, the shingled solar cell can includethe at least one first solar cell piece 11 of the first solar cell andthe at least one second solar cell piece 11′ of the second solar cell.The at least one first solar cell piece 11 and the at least one secondsolar cell piece 11′ overlap with each other. However, the presentdisclosure is not limited thereto and some of the adjacent solar cellpieces of the shingled solar cell can be from the same solar cell, suchas the first solar cell or the second solar cell. Adjacent solar cellpieces can overlap by less than 20%, specifically less than 10%, andmore specifically less than 5% of the total surface area, such as thefrontside surface or backside surface, of the solar cell pieces.

In some implementations, each solar cell piece of the plurality ofoverlapping solar cell pieces of the solar cell arrangement 20 can haveone or more conductive patterns, such as fingers 14 and/or busbars 13,provided thereon. As an example, the solar cell piece, such as the atleast one first solar cell piece 11, can have a frontside and a backsidecorresponding to the frontside and the backside, respectively, of theformer solar cell. Optionally, the solar cell piece can have one or morebackside contacts. As exemplarily shown in FIG. 2 , the at least onefirst solar cell piece 11 can have a first backside contact 15, and theat least one second solar cell piece 11′ can have a second backsidecontact 15′.

Adjacent solar cell pieces are electrically connected to each other inthe overlapping region. The solar cell pieces are thus connected inseries such that current generated by the individual solar cell piecesflows along the series of solar cell pieces to be collected, forexample, at an end portion of the solar cell arrangement 20 (not shown).The overlapping configuration can provide solar cell arrangements havingan increased output power. As an example, the busbar 13 provided on theat least one first solar cell piece 11 can be electrically connected tothe second backside contact 15′ of the at least one second solar cellpiece 11′. As shown in the example of FIG. 2 , the separation device canbe configured to separate the solar cell adjacent to the busbars of thesolar cell. In other words, each solar cell piece can have a busbar, andparticularly only one busbar, provided thereon, which can be located atan edge of the solar cell piece.

In some implementations, an adhesive 17, such as an electricallyconductive adhesive, can be provided to connect to solar cell pieces inthe overlapping region. According to some embodiments, which can becombined with other embodiments described herein, the apparatus formanufacture of at least two solar cell arrangements includes an adhesiveapplication device configured to apply the adhesive 17 to the solar cellor the solar cell pieces thereof, such as the two or more first pieces,before the two or more first solar cell pieces are positioned on thesupport device. Two solar cell pieces can be overlapped with theadhesive being provided at one solar cell piece of the two solar cellpieces such that the two solar cell pieces can be electrically andmechanically connected to each other. As an example, the adhesive can bein a substantially liquid form when the adhesive is applied to a solarcell or solar cell piece.

According to some embodiments, the adhesive application device can beconfigured to apply the adhesive 17 on at least a portion of theconductive line pattern, such as the busbars, of the solar cell or thesolar cell pieces thereof. In some implementations, the adhesive isapplied before the solar cell is divided into the two or more solar cellpieces. In other implementations, the adhesive is applied to the solarcell piece(s) after the solar cell has been divided into the two or morepieces.

According to some embodiments, the adhesive is selected from the groupconsisting of solder, silver paste, silicone-based electricallyconductive adhesive, and epoxy-based electrically conductive adhesive.

When pieces have been overlapped, for example, in the assembling of thesolar cell arrangement, a drying process can be performed to dry theadhesive. In some implementations, the drying process can include aheating of the overlapping region of the two solar cell pieces using,for example, a heater such as an infrared heater. The heater is furtherexplained with respect to FIG. 5 .

FIGS. 3A to C show schematic views of a separation device 110 accordingto embodiments described herein. FIGS. 3A and B show schematic sideviews, and FIG. 3C shows a schematic top view.

The separation device 110 is configured to separate a solar cell 10 intotwo or more solar cell pieces. In particular, the separation device 110can create smaller cells (solar cell pieces or solar cell elements)starting from the (big) solar cell. According to some embodiments, whichcan be combined with other embodiments described herein, the separationdevice 110 includes, or is, a cleaving device 111 configured tomechanically contact the solar cell 10 to divide the solar cell 10. Insome implementations, the cleaving device 111 includes a moveable body112 and a contact element 114 fixed to the moveable body 112. Thecleaving device 111 and the moveable body 112 can be provided asseparate entities, or can be integrally formed from a single piece ofmaterial, such as a plastic material.

The contact element 114 can be a blade or an element with a sharp tipconfigured to contact the solar cell 10 for cleaving and dividing thesolar cell 10. According to some embodiments, the contact element 114can be made of a plastic material. In some implementations, the moveablebody 112 can be configured to move the contact element 114 towards thesolar cell, for example, in a quick motion, in order to provide a sharpdividing line at the solar cell 10. For instance, a motor (e.g., anup-down motor such as a linear motor) of the separation device 110 canpush the moveable body 112 having the contact element 114 attachedthereto against the solar cell 10 in order to cleave the solar cell 10.According to some embodiments, the moveable body 112 can be movablesubstantially vertically towards and away from the solar cell 10.

According to some embodiments, the separation device 110 includes aholding device 118 configured for holding the solar cell 10 at a supportarrangement, such as a first support element 116 of the supportarrangement, during the separation process. By fixing the solar cell 10to the support arrangement using the holding device 118, a reliableseparation process can be provided. The holding device 118 can include,or be, a holding element configured to mechanically contact the solarcell 10, such as the frontside or backside of the solar cell 10, forholding down the solar cell 10 at the support arrangement.

In some implementations, the apparatus of the present disclosure, andparticularly to separation device 110, includes the support arrangementhaving the first support element 116 and optionally a second supportelement 117. The first support element 116 can be configured such thatthe solar cell 10 protrudes over an edge of the first support element116 during the separation process. As an example, the cleaving device111 can be configured to contact the solar cell 10 at a position awayfrom the edge of the first support element 116 to break the solar cellpiece off the solar cell 10, as it is exemplarily shown in FIG. 3B.

The solar cell piece that has been separated from the solar cell 10 canbe collected or cached by the second support element 117, which can beoffset with respect to the first support element 116, for example, inthe vertical direction. As an example, the solar cell piece can fallonto the second support element 117 when the solar cell piece has beenseparated from the solar cell 10.

In some implementations, the first support element 116 and/or the secondsupport element 117 can be belt conveyors configured for conveying thesolar cell 10 and/or solar cell pieces, as it is shown in the top viewof FIG. 3C. The first support element 116 and/or the second supportelement 117 can each have two or more belts spaced apart from eachother. In particular, a gap can be provided between the two or morebelts. In some embodiments, an inspection system can be provided, forexample, below the first support element 116 and/or the second supportelement 117 to determine, for example, a position of the solar cell 10and/or the solar cell pieces on the first support element 116 and/or thesecond support element 117. The gap between the two or more beltsensures that the inspection system, and particularly a camera thereof,can see the solar cell 10 or solar cell pieces located on the firstsupport element 116 and/or the second support element 117.

According to some embodiments, which can be combined with otherembodiments described herein, the separation device 110 includes atleast one solar cell perforation device. As an example, the at least onesolar cell perforation device includes, or is, a laser. As an example,the at least one solar cell perforation device can be configured toperforate the solar cell 10 before the solar cell 10 is separated intothe two or more solar cell pieces by the cleaving device 111.

The at least one solar cell perforation device can be configured togenerate one or more predetermined breaking points or lines on the solarcell 10 such that the solar cell 10 can be easily broke into the two ormore solar cell pieces. As an example, the at least one solar cellperforation device can be configured to provide a plurality ofpredetermined breaking points along a substantially straight line on thesolar cell that defines a separation line between two adjacent solarcell pieces. In another example, the at least one solar cell perforationdevice can be configured to provide a continuous predetermined breakingline on the solar cell 10 that defines the separation line between twoadjacent solar cell pieces. The perforation of the solar cell 10 beforethe cleaving action can provide for a straight and sharp edge at thesolar cell piece that is broke off the solar cell 10. In particular, forhypercell creation, the solar cell 10 can be previously lasered in orderto cleave the solar cell 10 into the smaller cells in a controlledmanner.

FIG. 4A shows a schematic side view of an apparatus for manufacture ofat least two solar cell arrangements according to further embodimentsdescribed herein. FIG. 4B shows a schematic top view of the apparatus.FIG. 5 shows a schematic view of overlapping solar cell pieces on asupport device 130 according to embodiments described herein.

According to some embodiments, which can be combined with otherembodiments described herein, the apparatus includes a transport device150 configured for transportation of the solar cell pieces of the solarcell(s), such as the two or more first solar cell pieces of the firstsolar cell. The transport device 150 can include, or be, a belt conveyorhaving a roller 154 rotatable around a first rotational axis 156 and oneor more first belts 152 provided on the roller 154. In someimplementations, the transport device 150 can have two or more beltsarranged in parallel and with gaps provided between the two or morebelts.

In some implementations, the first support element and/or the secondsupport element of the support arrangement of the separation devicedescribed with respect to FIGS. 3A to C can be provided by the transportdevice 150, and particularly by the one or more first belts 152. Theseparation device is not illustrated in FIGS. 4A and B.

According to some embodiments, the support device 130 of the apparatusfor manufacture of at least two solar cell arrangements according to theembodiments described herein can include, or be, a belt conveyor. Thesupport device 130, e.g., the belt conveyor, is configured to support,fix and transport the at least two solar cell arrangements, such as thefirst solar cell arrangement and the second solar cell arrangement. Inparticular, the support device 130 can be configured for transportationof the at least two solar cell arrangements in a transport direction 4,which can be a substantially horizontal direction (for example, see FIG.5 ).

The belt conveyor constituting the support device 130 can include aroller 136 rotatable around a second rotational axis 134 and one or moresecond belts 132 provided on the roller 136. In some implementations,the support device 130 can have two or more belts arranged in paralleland with gaps provided between the two or more belts. As an example,each belt of the two or more belts can be configured to support (only)one solar cell arrangement of the at least two solar cell arrangements(for example, see FIG. 8A). In other implementations, the support device130 has one single belt on which the at least two solar cellarrangements can be assembled in parallel (for example, see FIG. 8B).

According to some embodiments, which can be combined with otherembodiments described herein, the support device 130 includes, or is, atleast one of an electrostatic chuck and a vacuum chuck. Theelectrostatic chuck that can be used as the support device is furtherdescribed with respect to FIGS. 11 to 17 . The vacuum chuck can includea support surface configured to support the at least two solar cellarrangements, wherein the support surface can have at least one of holesand recesses connected to a suction device, such as a vacuum pump, inorder to generate an under pressure in the holes and/or recesses to holdthe solar cell arrangement at the support surface.

The at least one positioning device 120 is configured for moving ortransferring the solar cell pieces of the solar cell from, for example,the transport device 150 to the support device 130 (indicated withreference numeral 3). As an example, the positioning device 120 cansequentially grip or pick up the solar cell pieces from the transportdevice 150, move the solar cell pieces to the support device 130,optionally align the solar cell pieces, and release the solar cellpieces in a predetermined position. In particular, the positioningdevice 120 can be configured to arrange the solar cell pieces in anoverlapping manner to form the first solar cell arrangement and thesecond solar cell arrangement. While the at least two solar cellarrangements are assembled on the support device 130, the support device130, and particularly the one or more first belts having the (partially)assembled solar cell arrangements positioned thereon, can continuouslymove in the transport direction 4. A continuous manufacturing processcan be provided.

According to some embodiments, the apparatus includes a controller 140configured to control the at least one positioning device 120. Inparticular, the controller 140 can control a movement of the positioningdevice 120 to move a solar cell piece to assemble a solar cellarrangement to which the solar cell piece has been allocated. As anexample, the controller 140 can control the at least one positioningdevice 120 to move the solar cell piece to either the first solar cellarrangement or the second solar cell arrangement based on one or moreproperties (e.g., geometric and/or physical properties) of the piece,such as geometric shape, electrical properties, optical properties,printing quality, and any combination thereof.

According to some embodiments, which can be combined with otherembodiments described herein, the at least one positioning device 120includes a gripper 122 configured to grip and hold a solar cell piece,such as the two more first pieces of the first solar cell. The gripper122 can be selected from the group consisting of vacuum grippers,mechanical grippers, electrostatic grippers, electrodynamic grippers,and any combination thereof. Embodiments of the gripper 122 are furtherexplained with respect to FIGS. 6A and B.

In some implementations, the positioning device 120 is movable in atleast one of a first direction 1 and a second direction 2. The firstdirection 1 can be a substantially horizontal direction. The seconddirection 2 can be a substantially vertical direction. The positioningdevice 120 can be movable sequentially or simultaneously in at least oneof the first direction 1 and the second direction 2. By the movement inthe first direction 1 and the second direction 2, the solar cell pieceheld by the positioning device 120 can be moved to the support device130 for assembling of a solar cell arrangement, such as the first solarcell arrangement and/or the second solar cell arrangement.

As an example, the positioning device 120 can move in the seconddirection 2, for example, upwards, to pick up the solar cell piece fromthe transport device 150. The positioning device 120 can then move inthe first direction 1, for example, forwards, to move the solar cellpiece from the transport device 150 to the support device 130. Thepositioning device 120 can move in the second direction 2, for example,downwards, to place the solar cell piece on the support device 130. Thepositioning device 120 can then move in the second direction 2 and thefirst direction 1, for example, back to the transport device 150 to pickup another solar cell piece from the transport device 150. It is to beunderstood that the movement in the first direction 1 can be a movementin a forward direction and a backward direction. Likewise, the movementin the second direction 2 can be a movement in an upward direction and amovement in a downward direction.

The term “vertical direction” is understood to distinguish over“horizontal direction”. That is, the “vertical direction” relates to asubstantially vertical movement, wherein a deviation of a few degrees,e.g. up to 5° or even up to 10°, from an exact vertical direction isstill considered as a “substantially vertical direction”. The verticaldirection can be substantially parallel to the force of gravity.

In some implementations, the apparatus, and particularly the positioningdevice 120, can be configured for alignment of the solar cell piece heldby the positioning device 120 before the solar cell piece is put on thesupport device 130. The apparatus can use information acquired by aninspection system which can include, for example, a camera configured todetect a position and/or orientation of the solar cell piece, forexample, held by the positioning device 120.

In some implementations, the positioning device 120 is movable a plane,such as a substantially horizontal plane. Such a movement can also bereferred to as “Θ movement”. As an example, the positioning device 120can be configured to adjust or align an angular orientation of a solarcell piece held by the positioning device 120 in the plane. The angularorientation of the solar cell piece can be aligned, for example, withrespect to the support device 130 and/or another solar cell piece on thesupport device 130 with which the solar cell piece held by thepositioning device 120 is to be overlapped. The solar cell arrangementcan be accurately assembled, wherein a quality of the solar cellarrangement can be improved. In some implementations, the positioningdevice 120 can be configured to rotate the solar cell piece around asubstantially vertical rotational axis by about 180°. In particular,edge pieces of pseudo-square solar cells described with respect to FIG.7B can be brought into similar orientations. As an example, one edgepiece (e.g., the front or leading edge piece) of the pseudo-square solarcell is not rotated by about 180° and the other edge piece (e.g., theback or trailing edge piece) of the pseudo-square solar cell is rotatedby about 180° such that the geometric shapes of the edge pieces areequally oriented or aligned.

According to some embodiments, the positioning device 120 is tiltable,for example, with respect to the first direction 1 and/or a horizontalplane. As an example, the positioning device 120 can tilt the solar cellpiece held by the positioning device 120 to align an orientation of thesolar cell piece with respect to another solar cell piece on the supportdevice 130 with which the solar cell piece held by the positioningdevice 120 is to be overlapped. In particular, the backside or backsideplane of the solar cell piece held by the positioning device 120 can beoriented to be substantially parallel to a frontside or frontside planeof the other solar cell piece on the support device 130. In someimplementations, the positioning device 120 is configured to align abackside contact of the solar cell piece with respect to a frontsidecontact, such as a busbar, of another solar cell piece on the supportdevice 130 such that an electrical contact between the backside contactand the frontside contact can be established, for example, with anadhesive provided therebetween.

As shown in FIG. 5 , a plurality of solar cell pieces can be positionedon the support device 130 in an overlapping manner to form the solarcell arrangement, which can be a shingled solar cell. At least some ofthe plurality of pieces originate from at least two different solarcells. In particular, the solar cell pieces can be sorted andindividually be allocated to a respective solar cell arrangement, forexample, based on one or more properties, such as geometric and/orphysical properties, of the respective solar cell piece.

In some implementations, the support device 130 is a belt conveyorhaving the one or more second belts 132. A movement of the beltconveyor, and in particular of the one or more second belts 132, and amovement of the at least one positioning device 120 can be synchronizedwith each other, for example, during the assembling of the at least twosolar cell arrangements on the support device 130. Additionally oralternatively, a movement of the transport device 150, for example, theone or more first belts 152, and a movement of the at least onepositioning device 120 and/or the one or more second belts 132 can besynchronized with each other. By synchronizing at least some of themovements, a continuous process flow for assembling of the at least twosolar cell arrangements can be provided.

According to some embodiments, which can be combined with otherembodiments described herein, the apparatus further includes a heatingdevice 160, for example, at or above the support device 130. The heatingdevice 160 is configured to heat at least one of the solar cellarrangements on the support device 130, such as the first solar cellarrangement and/or the second solar cell arrangement. The heating device160 can be selected from the group consisting of conduction heaters(e.g., hot plates), convective heaters, resistive heaters, infraredheaters, lamp heaters, hot air heaters, and any combination thereof. Asan example, the support device 130 can be configured as a hot plate forconduction heat transfer to heat the solar cell arrangement(s) on thesupport device 130.

In some implementations, the heating device 160 can extend along atleast a portion of the support device 130, for example, in the transportdirection 4 in which the solar cell arrangements are conveyed by thesupport device 130. The heating device 160 can extend along a distancesufficient to dry the adhesive used for electrically connecting adjacentoverlapping solar cell pieces, such as the silver paste or solder. Theheating device 160 can have two or more heating elements provided inparallel at the support device 130. As an example, a first heatingelement can be configured to heat the first solar cell arrangement. Asecond heating element can be configured to heat the second solar cellarrangement. In particular, according to some embodiments, the heatingdevice 160 can extend above the support device 130 at positionscorresponding to positions of the at least two solar cell arrangements.As an example, the first heating element can be arranged above the firstsolar cell arrangement, and the second heating element can be arrangedabove the second solar cell arrangement.

The heating device 160 can be configured to provide a predeterminedtemperature at the position of at least a portion of the solar cellarrangement. The predetermined temperature can be at least 100° C.,specifically at least 150° C., and more specifically at least 300° C.The predetermined temperature can be in a range of between 100° C. and400° C., and can be specifically in a range of between 100° C. and 200°C.

FIGS. 6A and B show schematic views of a positioning device 220according to embodiments described herein.

According to some embodiments, which can be combined with otherembodiments described herein, the at least one positioning device 220includes one or more grippers 222 configured to grip and hold a solarcell piece, such as the two more first pieces of the first solar cell.The one or more grippers 222 can be selected from the group consistingof vacuum grippers, mechanical grippers, electrostatic grippers,electrodynamic grippers, and any combination thereof. The vacuum can usea suction force to hold the solar cell piece at the gripper. Themechanical gripper can use mechanical devices, such as clamps, to holdthe solar cell piece at the gripper. The electrostatic grippers andelectrodynamic grippers can use an electrostatic force and anelectrodynamic force, respectively, to hold the solar cell piece at thegripper.

In some implementations, at least one gripper, and particularly eachgripper, of the one or more grippers 222 can include one or more gripperelements 224. As an example, the gripper can include two or more, suchas three, four, five or six gripper elements 224 configured forcontacting and gripping a solar cell piece. As an example, the one ormore gripper elements 224 can be suction cups configured to provide anunder-pressure at a surface of the solar cell piece to hold the piecethat the one or more gripper elements 224.

According to some embodiments, each gripper of the one or more grippers222 is configured for holding and moving one solar cell piece. Infurther embodiments, each gripper of the one or more grippers 222 isconfigured for simultaneously holding and moving two or more solar cellpieces.

FIGS. 7A and B show schematic views of a full-square solar cell 70 and apseudo-square solar cell 80, respectively, according to embodimentsdescribed herein.

The full-square solar cell 70 can be, for example, a quadratic multicrystalline wafer cut from silicon ingots. The full-square solar cell 70having fingers 14 and busbars 13 provided thereon can be cleaved into aplurality of pieces, such as the three pieces 71, 72, and 73 which areexemplarily illustrated in FIG. 7A.

The pseudo-square solar cell 80 can be a squared wafer with roundededges 81 cut from monocrystalline silicon ingots. In comparison with thefull-square solar cell 70, the pseudo-square solar cell 80 can bebeneficial in that less waste is produced during the manufacturingprocess. The pseudo-square solar cell 80 can be cleaved into a pluralityof pieces, such as the three pieces 82, 83, and 84 exemplarilyillustrated in FIG. 7B.

The individual pieces of the solar cells can be allocated to differentsolar cell arrangements based on the geometric shape. As an example, the(edge) pieces of the pseudo-square solar cell 80 having the roundededges 81 (“pseudo-square pieces”) can be allocated to one solar cellarrangement, for example, the first solar cell arrangement. The (middle)piece(s), which are full-square pieces, can be allocated to anothersolar cell arrangement, for example, the second solar cell arrangement.Specifically, solar cell arrangements having only full-square pieces oronly pseud-square pieces are provided. “Bottlenecks” caused by apseud-square piece in a solar cell arrangement having otherwisefull-square pieces can be avoided and an efficiency of the solar cellarrangement can be increased. Particular, module power can be increased.According to some implementations, and as described with respect toFIGS. 4A, 4B and 5 , either the solar cell piece 82 or the solar cellpiece 84 can be rotated by about 180° such that both solar cell pieces,and particularly the rounded edges 81 thereof, are equally alignedbefore the solar cell arrangement is assembled.

According to some embodiments, which can be combined with otherembodiments described herein, the solar cells, such as the full-squaresolar cell 70 and/or pseudo-square solar cell 80, can be separated ordivided at positions adjacent to the busbars 13 of the respective solarcell. In other words, each solar cell piece can have a busbar, andparticularly only one busbar, provided thereon, which can be located atan edge of the solar cell piece.

FIG. 8A shows a schematic view of an apparatus 300 for manufacture of atleast two solar cell arrangements, such as shingled solar cells,according to an embodiment described herein.

According to some embodiments, which can be combined with otherembodiments described herein, the apparatus 300 can include one or moreinput conveyors, such as a first input conveyor 302 and a second inputconveyor 304, configured for inputting solar cells into the separationdevice 310. The one or more input conveyors can be parallel lanes forsimultaneously inputting a plurality of solar cells into the separationdevice 310. The one or more input conveyors can be belt conveyors.According to some embodiments, the transport device described withrespect to FIGS. 4A, 4B and 5 can be provided by the one or more inputconveyors.

According to some embodiments, the apparatus 300 further includes one ormore centering devices, such as one or more mechanical centeringdevices, configured to center or align the solar cells 10 which are tobe processed by the separation device 310. As an example, each inputconveyor of the one or more input conveyors can have a respectivecentering device. In particular, a first centering device can beprovided at the first input conveyor 302 and a second centering devicecan be provided at the second input conveyor 304.

In some implementations, the separation device 310 is configured forseparating a plurality of solar cells into solar cell pieces. Anexample, the separation device 310 is configured for separating at leastthe first solar cell into the two or more first solar cell pieces andthe second solar cell into the two or more second solar cell pieces. Asan example, the separation device 310 is configured for sequentially orsimultaneously separating the first solar cell and the second solar cellinto the two or more first solar cell pieces and the two or more secondsolar cell pieces, respectively.

In one example, the first solar cell and the second solar cell can besequentially inputted into the separation device 310 using, for example,the first input conveyor 302 or the second input conveyor 304. Theseparation device 310 can sequentially separate the first solar cell andthe second solar cell into the two or more first solar cell pieces andthe two or more second solar cell pieces, respectively. Each piece isthen allocated to a respective solar cell arrangement, for example,based on one or more properties, such as geometric and/or physicalproperties, of the solar cell piece.

In another example, the first solar cell and the second solar cell canbe simultaneously inputted into the separation device 310 using, forexample, the first input conveyor 302 and the second input conveyor 304.In particular, the first solar cell can be inputted using the firstinput conveyor 302 and the second solar cell can be inputted using thesecond input conveyor 304. The separation device 310 can substantiallysimultaneously separate the first solar cell and the second solar cellinto the two or more first solar cell pieces and the two or more secondsolar cell pieces, respectively. In other words, two or more solarcells, such as the first solar cell and the second solar cell, can besimultaneously inputted into, and cleaved by, the separation device 310for parallel production of a plurality of solar cell pieces from two ormore solar cells. Each solar cell piece is then allocated to arespective solar cell arrangement, for example, based on one or moreproperties of the solar cell piece.

Although two input conveyors are illustrated in the example of FIG. 8A,it is to be understood that the present disclosure is not limitedthereto and that one input conveyor or three, four or even more inputconveyors can be provided for (simultaneously) inputting a plurality ofsolar cells into the separation device 310.

According to some embodiments, the separation device 310 includes atleast a first cleaving device configured for separating the first solarcell into the two or more first solar cell pieces and a second cleavingdevice configured for separating the second solar cell into the two ormore second solar cell pieces. Specifically, the separation device 310can include two or more cleaving devices, such as the first cleavingdevice and the second cleaving device, for a simultaneous or parallelprocessing of two or more solar cells. Providing the parallelarrangement of the first cleaving device and the second cleaving devicecan be particularly beneficial when two or more solar cells aresimultaneously inputted into the separation device 310.

The positioning device 320 is configured for positioning the solar cellpieces provided by the separation device 310 on the support device 330for the parallel assembling of the at least two solar cell arrangements.In some implementations, the positioning device 320 is configured forpositioning at least one second solar cell piece of the one or moresecond solar cell pieces of the second solar cell on the support device330 for forming the first solar cell arrangement together with the atleast one first solar cell piece of the first solar cell, and isconfigured for positioning at least one other second solar cell piece ofthe two or more second solar cell pieces of the second solar cell on thesupport device 330 for forming the second solar cell arrangementtogether with the at least one other first solar cell piece.

As an example, solar cell pieces of the solar cells sequentially orsimultaneously processed by the separation device 310 and having a firstpredetermined property, such as a first predetermined geometric shape,can be arranged to form one solar cell arrangement, for example, thefirst solar cell arrangement. Solar cell pieces of solar cellssequentially or simultaneously processed by the separation device 310and having a second predetermined property, such as a secondpredetermined geometric shape, can be arranged to form another solarcell arrangement, for example, the second solar cell arrangement. Forinstance, the (edge) pieces of the pseudo-square solar cell having therounded edges (“pseudo-square pieces”) can have the first predeterminedgeometric shape. The (middle) piece(s), which are full-square pieces,can have the second predetermined geometric shape. Accordingly, solarcell arrangements having either only pseudo-square pieces or onlyfull-square pieces can be assembled. Full-square pieces can originatefrom both, pseudo-square solar cells and full-square solar cells.

According to some embodiments, which can be combined with otherembodiments described herein, the support device 330 can have two ormore support units arranged in parallel. The two or more support unitscan be separated from each other. Each support unit of the two or moresupport units can be configured to support a respective solar cellarrangement of the at least two solar cell arrangements. As an example,a first support unit 332 can be configured to support the first solarcell arrangement and a second support unit 334 can be configured tosupport the second solar cell arrangement. The support device 330 caninclude further support units, such as a third support unit 336 and thefourth support unit 338 configured to support further solar cellarrangements.

As an example, solar cell pieces of solar cells inputted via the firstinput conveyor 302 can be allocated to solar cell arrangements on thefirst support unit 332 and the second support unit 334. Solar cellpieces of solar cells inputted via the second input conveyor 304 can beallocated to solar cell arrangements on the third support unit 336 andthe fourth support unit 338. In this example, the first support unit 332and the second support unit 334 can be operated independently from thethird support unit 336 and the fourth support unit 338. Likewise, thefirst input conveyor 302 and the cleaving procedure of the solar cellsinputted via the first input conveyor 302 can be operated independentlyfrom the second input conveyor 304 and the cleaving procedure of thesolar cells inputted via the second input conveyor 304. A throughput ofthe apparatus 300 can be increased, since malfunctions have a localizedeffect and do not lead to a stop of the whole production process.

In further examples, solar cell pieces of solar cells inputted via thefirst input conveyor 302 can be allocated to solar cell arrangements onany one of the two or more support units, such as the first to fourthsupport units. Likewise, solar cell pieces of solar cells inputted viathe second input conveyor 304 can be allocated to solar cellarrangements on any one of the two or more support units, such as thefirst to fourth support units.

According to some embodiments, the support device 330 includes the atleast a belt conveyor, wherein the at least a belt conveyor includes twoor more belt conveyor spaced apart from each other. As an example, afirst belt conveyor is configured to support the first solar cellarrangement and a second belt conveyor spaced apart from the first beltconveyor is configured to support the second solar cell arrangement. Insome implementations, the two or more support units are belt conveyorsarranged in parallel. As an example, the first support unit 332 is thefirst belt conveyor, the second support unit 334 is the second beltconveyor, the third support unit 336 is a third belt conveyor, and thefourth support unit 338 is a fourth belt conveyor. The first to fourthbelt conveyors can be arranged in parallel.

In some implementations, a movement of the support device 330 providedby the belt conveyor and a movement of the at least one positioningdevice 320 are synchronized or correlated with each other. As anexample, a movement of the first input conveyor 302, a cleaving processof the solar cells inputted via the first input conveyor 302, anoperation of the positioning device 320, and a movement of the firstsupport unit 332 and the second support unit 334 are synchronized orcoordinated. Likewise, a movement of the second input conveyor 304, acleaving process of the solar cells inputted via the second inputconveyor 304, an operation of the positioning device 320, and a movementof the third support unit 336 and the fourth support unit 338 aresynchronized or coordinated.

According to some embodiments, which can be combined with otherembodiments described herein, the apparatus 300 is configured toallocate each solar cell piece of the solar cells to a respective solarcell arrangement based on one or more properties, such as geometricand/or physical properties, of the solar cell piece. As an example, theapparatus 300 is configured to allocate each solar cell piece of the twoor more first for pieces of the first solar cell to either the firstsolar cell arrangement or the second solar cell arrangement based on oneor more properties of the respective solar cell piece of the two morefirst solar cell pieces. Likewise, the apparatus 300 can be configuredto allocate each solar cell piece of the two or more second solar cellpieces of the second solar cell to either the first solar cellarrangement or the second solar cell arrangement based on one or moreproperties of the respective solar cell piece of the two more secondsolar cell pieces.

The one or more properties can be determined before the solar cell iscleaved into the solar cell pieces and/or after the solar cell has beencleaved into the solar cell pieces. In the former case, measurements,such as electrical measurements, of the whole solar cell can beperformed. In the latter case, measurements, such as electroluminescenceand/or photoluminescence measurements, of the individual solar cellpieces can be performed.

The one or more properties can be based on metrology. As an example, theone or more properties, such as the one or more geometric and/orphysical properties, can be selected from the group consisting ofgeometric shape, electrical properties, optical properties, printingquality, and any combination thereof. The geometric shape can be, forexample, “pseudo-square” and/or “full square”, as explained with respectto FIGS. 7A and B. As an example, the (edge) pieces of a pseudo-squaresolar cell having the rounded edges (“pseudo-square pieces”) can beallocated to one solar cell arrangement, for example, the first solarcell arrangement. The (middle) piece(s), which are full-square pieces,can be allocated to another solar cell arrangement, for example, thesecond solar cell arrangement.

The electrical properties, optical properties or combined electrical andoptical properties can be selected from the group consisting ofelectroluminescence, photoluminescence, and electrical characteristics.As an example, at least one of electroluminescence measurements,photoluminescence measurements, and electrical measurements (e.g.,measurements of a current-voltage (I-V) curve of the solar cell) can beperformed before the solar cell is cleaved into the solar cell pieces.Additionally or alternatively, at least one of electroluminescencemeasurements and photoluminescence measurements can be performed foreach solar cell piece after the solar cell has been cleaved into saidsolar cell pieces.

Additionally or alternatively to the above electrical properties,optical properties or combined electrical and optical properties, atleast one of a printing quality and structural integrity of the solarcell and/or the solar cell pieces can be performed. As an example, aprinting quality and/or structural integrity can be determined beforethe solar cell is cleaved into the solar cell pieces. Additionally oralternatively, printing quality and/or structural integrity can bedetermined for each solar cell piece after the solar cell has beencleaved into said solar cell pieces. The determining of the printingquality may include a determining of a quality (e.g., accuracy, linethickness, lined width, and like) of a conductive line pattern of thesolar cell, for example, of fingers and/or busbars.

Using the one or more properties of the individual solar cell pieces forallocating the solar cell pieces to solar cell arrangements can ensurethat each solar cell arrangement includes only solar cell pieces ofsimilar characteristics. Bottlenecks that would, for example, reduce amodule power can be avoided.

According to some embodiments, which can be combined with otherembodiments described herein, the apparatus 300 includes at least one ofa first inspection device, a second inspection device, and a thirdinspection device. The first inspection device, the second inspectiondevice, and the third inspection device can be configured to determineand/or measure at least one of the above mentioned properties of thesolar cell, solar cell pieces and/or solar cell arrangement. Inparticular, the one or more properties, such as the geometric and/orphysical properties, can be selected from the group consisting ofgeometric shape, electrical properties, optical properties, printingquality, and any combination thereof.

In some implementations, the first inspection device is configured tomeasure and/or determine one or more properties of a solar cell beforethe solar cell is separated into two or more solar cell pieces. As anexample, the first inspection device is configured to measure and/ordetermine one or more properties of the first solar cell before thefirst solar cell is separated into the two or more first pieces.According to some embodiments, the second inspection device isconfigured to measure and/or determine one or more properties of atleast some of the solar cell pieces, such as the two or more first solarcell pieces of the first solar cell, after the solar cell has beenseparated into said solar cell pieces. According to some embodiments,the third inspection device is configured to measure and/or determineone or more properties of at least one solar cell arrangement of the atleast two solar cell arrangements, such as the first solar cellarrangement and/or the second solar cell arrangement.

According to some embodiments, which can be combined with otherembodiments described herein, the apparatus 300 further includes asorting device configured for sorting the at least two solar cellarrangements, such as the first solar cell arrangement and the secondsolar cell arrangement, based to a quality determination of the at leasttwo solar cell arrangements. As an example, the sorting device isconfigured for sorting the at least two solar cell arrangements based oninformation received from the third inspection device. In particular,solar cell arrangements which are defective or have a low quality can bediscarded. Optionally, defective solar cell arrangements can undergo areworking or repair process, for example, to replace defective orlow-quality solar cell pieces.

FIG. 8B shows a schematic view of an apparatus 400 for manufacture of atleast two solar cell arrangements according to a further embodimentdescribed herein. The apparatus 400 of FIG. 8B is similar to theapparatus described with respect to FIG. 8A, and a description ofsimilar or identical aspects is not repeated.

According to some embodiments, the support device 430 is a belt conveyorhaving one single belt on which the at least two solar cell arrangementscan be assembled in parallel. In the example of FIG. 8B, three solarcell arrangements are assembled in parallel. As an example,pseudo-square solar cell can be inputted via the two or more inputconveyors, such as the first input conveyor 302 and the second inputconveyor 304. Each pseudo-square solar cell can be divided into, forexample, four solar cell pieces. That is, each pseudo-square solar cellis divided into two edge pieces having the rounded edges and two middlepieces, which are full-square pieces.

The edge pieces of the pseudo-square solar cell inputted via the two ormore input conveyors can be allocated to the middle solar cellarrangement of the three solar cell arrangements using the positioningdevice 420. The middle pieces, which are full-square pieces, can beallocated to outer two solar cell arrangements of the three second solarcell arrangements. A same number of solar cell pieces can be allocatedto each solar cell arrangement of the three solar cell arrangements, andthe solar cell arrangements can be assembled at the same speed.

FIG. 8C shows a schematic view of an apparatus for manufacture of atleast two solar cell arrangements according to a yet further embodimentdescribed herein. The apparatus of FIG. 8C is similar to the apparatusesdescribed with respect to FIGS. 8A and B, and a description of similaror identical aspects is not repeated.

According to some embodiments, which can be combined with otherembodiments described herein, the apparatus has a positioningarrangement including a displacement device 450 and the positioningdevice 455 described before. The displacement device 450 can beconfigured to laterally displace solar cell pieces provided by theseparation device 310, for example, by the first cleaving device and thesecond cleaving device. In some implementations, the apparatus can havea plurality of parallel transport lanes provided at the separationdevice 310 and/or the positioning device 455. The plurality of transportlanes can be configured for transportation of the solar cell piecesafter the cleaving process and prior to the positioning of the solarcell pieces on the support device 430. The plurality of transport lanescan be belt conveyors. In some implementations, the plurality oftransport lanes can include two outer transport lanes 460 and a centertransport lane 465.

In some embodiments, the two outer transport lanes 460 can be aligned(e.g., in line) with the first input conveyor 302 and the second inputconveyor 304, respectively. The center transport lane 465 can bepositioned between the first input conveyor 302 and the second inputconveyor 304. In particular, selected solar cell pieces, such as thesolar cell pieces (e.g., the edge pieces of the pseudo-square solarcells) used for assembling of the middle solar cell arrangement can bepicked up by the displacement device 450 of the positioning device 455to move or transfer the selected solar cell pieces after the cleavingprocess to the center transport lane 465. The outer transport lanes 460can be configured for transportation of the middle pieces of thepseudo-square solar cells, which are full-square pieces.

It is to be understood that the plurality of transport lanes between theseparation device and the positioning device/support device as describedwith respect to FIG. 8C can be similarly implemented in the apparatusdescribed with respect to FIGS. 8A and B.

FIG. 9A shows a schematic view of a system 500 for manufacture of atleast two shingled solar cells according to embodiments describedherein. The system 500 can be part of, or constitute, a production linefor shingled solar cells.

The system 500 includes the apparatus for manufacture of at least twosolar cell arrangements, which are shingled solar cells, according tothe embodiments described herein. The system 500 further includes aproduction tool 510 for manufacturing a plurality of solar cellsincluding the first solar cell. The plurality of solar cells are inputinto the apparatus. The apparatus includes the separation device 530,the positioning device 540, and the support device 550 according to theembodiments described therein.

In some implementations, the production tool 510 includes one or moreprinting devices configured for printing one or more conductive lines onsolar cell substrates used in the manufacture of the plurality of solarcells. The one or more conductive lines are selected from fingers andbusbars. The one or more printing devices can be configured for doubleprinting of the one or more conductive lines. Specifically, the one ormore printing devices can be configured for double printing of at leastone of the fingers and busbars.

According to some embodiments, the system 500, and particularly theapparatus, includes an adhesive application device 520 configured toapply an adhesive to the solar cell before the solar cell is separatedinto the two or more solar cell pieces. The adhesive is applied toportions of the solar cell corresponding to an overlapping regionbetween two adjacent solar cell pieces that are arranged on the supportdevice 550 in the overlapping manner. According to some embodiments, theadhesive application device 520 can be configured to apply the adhesiveon at least a portion of the conductive line pattern, such as thebusbars, of the solar cell.

According to some embodiments, which can be combined with otherembodiments described herein, the separation device 530 includes the atleast one solar cell perforation device. As an example, the at least onesolar cell perforation device includes, or is, a laser. As an example,the at least one solar cell perforation device can be configured toperforate the solar cell before the solar cell is separated into the twoor more solar cell pieces.

In some implementations, the system 500 further includes a heatingdevice 560, for example, subsequent to, or above, the support device 550of the apparatus. An embodiment of the heating device 560 is describedwith respect to FIG. 5 . In particular, the heating device 560 isconfigured to heat at least one of the solar cell arrangements to drythe adhesive in the overlapping region between two adjacent solar cellpieces. The heating device 560 can be selected from the group consistingof conduction heaters (e.g., hot plates), convective heaters, resistiveheaters, infrared heaters, lamp heaters, hot air heaters, and anycombination thereof.

According to some embodiments, which can be combined with otherembodiments described herein, the system 500 includes a sorting device570 configured for sorting the at least two solar cell arrangements,such as the first solar cell arrangement and the second solar cellarrangement, based on a quality determination of the at least two solarcell arrangements. As an example, solar cell arrangements which aredefective or have a low quality can be discarded. Optionally, defectivesolar cell arrangements can undergo a reworking or repair process, forexample, to replace defective or low-quality solar cell pieces

FIG. 9B shows a schematic view of a system 600 for manufacture of atleast two shingled solar cells according to further embodimentsdescribed herein. The system 600 is similar to the system described withrespect to FIG. 9A and a description of similar or identical aspects isnot repeated. In particular, the system 600 includes the production tool510, the adhesive application device 520, the apparatus, the heatingdevice 560, and the sorting device 570.

According to some embodiments, which can be combined with otherembodiments described herein, the system 600 includes an inspectionarrangement. The inspection arrangement can include at least one of afirst inspection device 615, a second inspection device (may be includedin the apparatus, for example, in the positioning device 540), and athird inspection device 665. The first inspection device 615, the secondinspection device, and the third inspection device 665 can be configuredto determine and/or measure one or more properties, such as geometricand/or physical properties, of at least one of the solar cell, solarcell pieces and/or solar cell arrangement as described with respect tothe embodiments described herein. In particular, the one or moreproperties can be selected from the group consisting of geometric shape,electrical properties, optical properties, printing quality, and anycombination thereof.

In some implementations, the first inspection device 615 is configuredto measure and/or determine one or more properties of a solar cellbefore the solar cell is separated into two or more solar cell pieces.Although the first inspection device 615 is exemplarily illustrated asbeing positioned between the production tool 510 and the adhesiveapplication device 520, the present disclosure is not limited thereto.An example, the first inspection device 615 can be provided between theadhesive application device and the separation device 530 or can beintegrated into the production tool 510, the adhesive application device520, or the separation device 530.

According to some embodiments, the second inspection device isconfigured to measure and/or determine one or more properties of atleast some of the solar cell pieces after the solar cell has beenseparated into pieces. The second inspection device can be integratedinto the apparatus, for example, in the separation device 530 or thepositioning device 540. In further implementations, the secondinspection device can be provided as a separate entity.

In some embodiments, the third inspection device 665 is configured tomeasure and/or determine one or more properties of the at least twosolar cell arrangements, such as the first solar cell arrangement and/orthe second solar cell arrangement. Although the third inspection device665 is exemplarily illustrated as being positioned between the heatingdevice 560 and the sorting device 570, the present disclosure is notlimited thereto. An example, the third inspection device 665 can beprovided at the support device 550. In some implementations, the supportdevice 550, the heating device 560, and the third inspection device 665are integrated in a single entity or process station.

FIG. 10 shows a flow chart of a method 1000 for manufacture of at leasttwo solar cell arrangements, such as shingled solar cells, according toembodiments described herein. The method 1000 can use the apparatusesand systems according to the embodiments described herein. Likewise, theapparatuses and systems of the present disclosure can be configured toimplement the method 1000.

The method 1000 includes in block 1100 a separating of each solar cellof one or more solar cells into two or more solar cell pieces, and inblock 1200 a forming of at least a first solar cell arrangement and asecond solar cell arrangement of the at least two solar cellarrangements from the two or more solar cell pieces. Each solar cellpiece of the two or more solar cell pieces is allocated to the firstsolar cell arrangement or the second solar cell arrangement based on oneor more geometric and/or physical properties of the solar cell piece. Insome implementations, the one or more solar cells are selected from thegroup consisting of full-square solar cells and pseudo-square solarcells.

In some implementations, the solar cells can be centered using, forexample, the centering device, to adjust a position of the solar cellsbefore the solar cells are cleaved into the two or more solar cellpieces. Optionally, an inspection system, such as the second inspectiondevice, can be used for an alignment of the solar cell pieces held, forexample, by the positioning device, before the solar cell piece is puton the support device. Information acquired by the inspection system canbe used for closed-loop control and a positioning of subsequent solarcell pieces.

According to some embodiments, the one or more geometric and/or physicalproperties are selected from the group consisting of geometric shape,electrical properties, optical properties, and any combination thereof.The one or more geometric and/or physical properties can be determinedusing at least one of the first inspection device, the second inspectiondevice and the third inspection device according to the embodimentsdescribed herein.

In some implementations, solar cell pieces of the two or more solar cellpieces corresponding to a predetermined geometric shape are allocated toeither the first solar cell arrangement or the second solar cellarrangement. The predetermined geometric shape can correspond to theedge pieces of the pseudo-square solar cells having the rounded edges,the middle pieces of the pseudo-square solar cells, or the solar cellpieces provided by the full-square solar cells, which are full-squaresolar cell pieces. As an example, the edge pieces of the pseudo-squaresolar cells having the rounded edges can correspond to a firstpredetermined geometric shape, the middle pieces of the pseudo-squaresolar cells can correspond to a second predetermined geometric shape,and the solar cell pieces provided by the full-square solar cells, whichare full-square solar cell pieces, can correspond to a thirdpredetermined geometric shape.

According to some embodiments, which can be combined with otherembodiments described herein, a geometric shape of the solar cell piecescan be determined or examined, for example, using the second inspectiondevice. In particular, it can be determined whether the edges of thesolar cell pieces have irregularities, for example, caused by thecleaving process. Solar cell pieces having such irregularities caneither be discarded or can be allocated to a low-quality solar cellarrangement.

In some embodiments, the method 1000 further includes a determining ofthe one or more geometric and/or physical properties at least one ofbefore the separating of each solar cell and after the forming of thefirst solar cell arrangement and the second solar cell arrangement. Asan example, the determining of the one or more geometric and/or physicalproperties before the separating of each solar cell can be conducted bythe first inspection device. The determining of the one or moregeometric and/or physical properties after the forming of the firstsolar cell arrangement and the second solar cell arrangement can beconducted by the third inspection device.

According to some embodiments, which can be combined with otherembodiments described herein, each solar cell of the one or more solarcells is separated into two, three, four, five, six, or more solar cellpieces. The number of solar cell pieces into which each solar cell isseparated can be selected according to at least one of a type of thesolar cell (e.g., pseudo-full square or full-square), a number of solarcell arrangements that are to be assembled in parallel, and aconfiguration of the support device (e.g., one single belt or multiplesupport units having separate belts).

In some implementations, the method 1000 further includes a gripping ofthe two or more solar cell pieces and a positioning of the two or moresolar cell pieces on the support device to form the first solar cellarrangement and the second solar cell arrangement. The gripping can beperformed using the positioning device as described, for example, withrespect to FIGS. 4 and 6 . In particular, a suction force provided by avacuum gripper can be used to pick up the solar cell piece.

According to some embodiments, the method 1000 further includes anapplying of an adhesive to the solar cell or the two or more solar cellpieces before positioning the two or more solar cell pieces on thesupport device. In particular, the adhesive can be applied in theoverlapping region of two adjacent solar cell pieces. According to someembodiments, the adhesive is an electrically conductive adhesiveselected from the group consisting of solder, silver paste, andelectrically conductive silicone adhesive. In some implementations, themethod 1000 can include a drying of the adhesive while the two or morepieces are fixed to, or held on, the support device. The drying can beperformed using the heating device, such as an infrared heater. Theheating device can be provided at the support device and can heat thesolar cell arrangement while the solar cell arrangement is moved ortransported below the heating device.

According to some embodiments, which can be combined with otherembodiments described herein, the following sequence can be used in themanufacture of the solar cell arrangement, such as the shingled solarcell.

a) using a laser (separator device) for perforation of the solar cells

b) inspection for quality check of solar cells before separating withthe separation device (separator)

c) applying an adhesive (conductive glue/paste deposition)

d) cleaving (separation into a plurality of pieces)

e) inspection for quality check after separator (optional)

f) inspection with cameras for alignment

g) positioning of solar cell pieces on support device (belt; hypercellformation)

h) heating (e.g., with lamps or resistors)

i) hypercell inspection for classification

It is to be understood that the above sequence is only an example, andthat process aspects can be arranged in a different order, one or moreprocess aspects can be omitted, and/or one or more process aspects canbe added.

According to embodiments described herein, the method for manufacture ofat least two solar cell arrangements can be conducted using computerprograms, software, computer software products and the interrelatedcontrollers, which can have a CPU, a memory, a user interface, and inputand output devices being in communication with the correspondingcomponents of the apparatus for processing a large area substrate.

FIG. 11 shows a schematic side view of a support device, which is anelectrostatic support device 900, according to embodiments describedherein. The electrostatic support device 900 can be used in theapparatus for manufacture of at least one solar cell arrangementaccording to the embodiments described herein.

As exemplarily shown in FIG. 11 , the support device 900 is configuredfor conveying at least one solar cell element 910 (the terms “solar cellelement” and “solar cell piece” are used synonymously throughout thepresent disclosure) in a transport direction 911. In particular, thesupport device includes a support element 920 (e.g., the belt)configured for supporting the at least one solar cell element 910. Forexample, the support element 920 may be a belt conveyor as exemplarilyshown in FIG. 11 . Typically, the support device 900 includes a firstrotatable roller 901 and a second rotatable roller 902 for moving thesupport element 920 in the transport direction 911. Further, accordingto embodiments described herein, the support device includes an electricarrangement 950 configured for providing an electrostatic force forholding the at least one solar cell element 910 on the support element920. In particular, the electrostatic force may act between the supportelement 920 and the at least one solar cell element 910.

Accordingly, a support device is provided which may beneficially be usedfor holding and conveying photovoltaic panel elements during production,e.g. during drying or serigraphic processes. In particular, embodimentsof the electrostatic support device as described herein provide analternative for conventional vacuum holding devices.

Accordingly, beneficially embodiments of the support device as describedherein provide for a simplified construction compared to vacuum holdingdevices because a complicated vacuum supply system can be omitted.Further, providing a support device having a belt conveyor as supportelement may particularly be beneficial for moving transport thinsheet-like elements, e.g. solar cell pieces or elements, betweendifferent processing stations in a continuous mode.

In the present disclosure, the term “support device” is to be understoodas a device which is configured for supporting an element, for example asheet like element such as a solar cell piece or solar cell arrangement.In particular, a “support device” as described herein may be understoodas a device which is configured for supporting an element in asubstantially horizontal orientation. In this regard, a “horizontalorientation” may be understood as an orientation in which theorientation of the longitudinal axis of the element supported by thesupport device deviates from an orientation which is perpendicular tothe direction of gravitational force by ±10° or less, particularly by±5° or less, more particularly by ±2° or less.

With exemplarily reference to FIG. 11 , according to embodiments whichcan be combined with any other embodiments described herein, the supportdevice 900 can include at least one first roller 901 and at least onesecond roller 902 configured for moving the support element 920 in thetransport direction 911. In particular, as indicated by the arrowsaround the axis of the first roller 901 and the second roller 902, thefirst roller 901 and the second roller 902 may be rotatable in order tomove the support element 920, particularly the conveyor belt, in thetransport direction 911. For example, the first roller 901 and/or thesecond roller 902 may be connected to a drive in order to provide arotational movement. Typically, the outer surfaces of the first roller901 and the second roller 902 are in contact with the support element920 in order to provide a frictional force between the first roller 901and the support element 920 as well as between the second roller 902 andthe support element 920. Accordingly, by rotation of the first roller901 and the second roller the support element 920 may be moved in thetransport direction 911, as exemplarily indicated in FIG. 11 .

In the present disclosure, the term “support element” is to beunderstood as an element of the support device which is configured forsupporting or holding a sheet-like element such as a solar cell element.In particular, the “support element” as described herein may beconfigured for providing a flat contact surface for the sheet-likeelement to be supported. In this regard, it is to be understood that theorientation of the flat contact surface may be horizontal, i.e. beingperpendicular to the direction of gravitational force within a range of±10° or less, particularly within a range of ±5° or less, moreparticularly within a range of ±2° or less. Typically, a “supportelement” as described herein may have a flexible structure, such thatthe support element can be employed as a conveyer belt which is guidedby one or more rollers in order to move the support element in atransport direction, as exemplarily described above with reference toFIG. 11 .

With exemplary reference to FIG. 11 , according to embodiments which canbe combined with any other embodiments described herein, the electricarrangement 950 includes a charging source 951 configured for providingan electrostatic charge to the support element 920. For example, thecharging source 951 may be arranged in proximity to the support element920. In particular, as exemplary indicated in FIG. 11 , the chargingsource 951 may be arranged relative to the support element 920 within adistance D of D≤10 mm, particularly D≤5 mm, more particularly D≤2 mm.

According to embodiments which can be combined with any otherembodiments described herein, the charging source 951 may be a voltagesource configured for providing a voltage of at least 5 kV, particularlyat least 8 kV, for example 10 kV±1 kV. In particular, the chargingsource 951 may be connected to a controller configured for controllingthe voltage, e.g. within a voltage range from 5 kV to 11 kV.

Accordingly, it is to be understood that according to embodimentsdescribed herein the charging source 951 is configured for providing anelectrostatic induction to the support element 920 in order to build upan electrostatic force on the support element 920 for holding asheet-like element, e.g. at least one solar cell element, on the supportelement 920.

According to some embodiments, the support device 900 may be a monopolarelectrostatic support device. In particular, in the present disclosure a“monopolar electrostatic support device” may be understood as a supportdevice having one or more charging sources which provide an electriccharge of the same electric polarity to the support element 920. Forexample, according to embodiments which can be combined with any otherembodiment described herein, a positive voltage may be applied to theone or more charging sources such that a negative charge is induced tothe support element, particularly on the surface of the support element.Alternatively, a negative voltage may be applied to the one or morecharging sources such that a positive charge is induced to the supportelement, particularly on the surface of the support element.

According to other embodiments, the support device 900 may be a bipolarelectrostatic support device. In particular, in the present disclosure a“bipolar electrostatic support device” may be understood as a supportdevice having two or more charging sources which provide an electriccharge of different electric polarity to the support element 920. Forexample, according to embodiments which can be combined with any otherembodiment described herein, a positive voltage may be applied to afirst charging source of the one or more charging sources and a negativevoltage may be applied to a second charging source of the one or morecharging sources. Accordingly, corresponding negatively charged regionsand corresponding positively charged regions may be generated at thesupport element, particularly at the surface of the support element byelectrostatic induction.

According to embodiments which can be combined with any otherembodiments described herein, the electric arrangement 950 includes anelectrical grounding for grounding the support element 920. For example,the electrical grounding may be provided by at least one roller of thefirst roller 901 and the second roller 902. Additionally oralternatively, the electrical grounding may be provided by a separategrounding roller 903 configured for grounding the support element 920,as exemplary shown in FIG. 11 . For example, the grounding roller 903may be arranged in between the first roller 901 and the second roller902. In particular, the grounding roller 903 may be arranged forcontacting a surface of the support element 920, as exemplary shown inFIG. 11 . Typically, the grounding roller 903 is arranged, such that theouter surface of the grounding roller is in contact with an innersurface of the support element. In this regard, it is to be understoodthat the “inner surface of the support element” is a surface of thesupport element which is opposite to the outer surface of the supportelement which contacts the at least one solar cell element beingsupported by the support element.

With exemplary reference to FIG. 12 , according to embodiments which canbe combined with any other embodiments described herein, the electricarrangement 950 of the support device 900 includes at least oneconductive arrangement 960 configured for receiving an electrostaticcharge from the charging source 951. In particular, the at least oneconductive arrangement 960 is configured for providing the electrostaticforce for holding the at least one solar cell element 910 on the supportelement 920. For example, the at least one conductive arrangement 960may be attached to or incorporated within the support element 920.

Accordingly, in the present disclosure, the term “electric arrangement”is to be understood as an arrangement including a conductive arrangementwhich is attached to or incorporated within the support element 920.Accordingly, in the present disclosure a “conductive arrangement” is tobe understood as an arrangement of conductive elements, e.g. wires ofconductive material such as copper, configured for receiving anelectrostatic charge from a charging source as described herein.Accordingly, an electrostatic force for holding the at least one solarcell element on the support element can be provided by the conductivearrangement as described herein.

With exemplary reference to FIG. 12 , according to embodiments which canbe combined with any other embodiments described herein, the at leastone conductive arrangement 960 may include a first busbar 961 and/or asecond busbar 962. In particular, the first busbar 961 and/or the secondbusbar 962 may be arranged parallel to the transport direction 911, asexemplary shown in FIG. 11 . According to some embodiments which can becombined with other embodiments described herein, the first busbar 961and/or the second busbar 962 are made of conductive material, e.g.copper wire, and are configured to transfer a charge to the supportelement 920. For example, in the case of a bipolar configuration of thesupport device two first rollers 901A, 901B and two second rollers 902A,902B may be provided, as exemplary shown in FIG. 12 . In particular, afirst pair of a first roller 901A and a second roller 902A may beelectrically connected by the first busbar 961 and a second pair of afirst roller 901B and a second roller 902B may be electrically connectedby the second busbar 962. In order to supply an electrical charge ofpositive polarity to the first busbar 961, the first pair of firstroller 901A and second roller 902A may be provided with inside rotaryjoints with sliding contacts for supplying a voltage of +5 kV or less,e.g. +4 kV. Accordingly, in order to supply an electrical charge ofnegative polarity to the second busbar 962, the second pair of firstroller 901B and second roller 902B may be provided with inside rotaryjoints with sliding contacts for supplying a voltage of −5 kV or less,e.g. −4 kV.

According to embodiments which can be combined with any otherembodiments described herein, the at least one conductive arrangement960 may include at least one electrode arrangement, e.g. a firstelectrode arrangement 971 and/or a second electrode arrangement 972 asexemplarily shown in FIGS. 14A and 14B. For example, the first electrodearrangement 971 may be electrically connected to the first busbar 961and the second electrode arrangement 972 may be electrically connectedto the second busbar 962. According to some embodiments, the firstelectrode arrangement 971 and/or the second electrode arrangement 972may be provided within at least one flexible panel 940, as exemplarilyshown in FIGS. 12, 14A and 14B.

According to embodiments which can be combined with any otherembodiments described herein, the support element 920 may includemultiple flexible panels which can be provided along the length of thesupport element 920, as exemplarily shown in FIG. 12 . As shown in FIG.12 , the multiple flexible panels may be arranged parallel to each otheralong the length of the support element. Further, the support element920 may be provided with markers which may be beneficial for mountingthe flexible panels onto the support element at preselected positions.

According to embodiments which can be combined with any otherembodiments described herein, the first busbar 961 may be arrangedwithin the support element 920 such that first contact regions 965A forproviding an electrical contact between the first busbar 961 and thefirst electrode arrangement 971 is provided. Accordingly, the secondbusbar 962 may be arranged within the support element 920 such thatsecond contact regions 965B for providing an electrical contact betweenthe second busbar 962 and the second electrode arrangement 972 isprovided. For example, as exemplary shown in FIG. 13 , the first busbar961 and/or the second busbar 962 may be arranged within the supportelement 920, such that a first portion 961A of the first busbar 961and/or a first portion 962A of the second busbar 962 are/is exposed tothe surface of the support element 920 to which the flexible panels 940may be mounted. Further, the first busbar 961 and/or the second busbar962 may be arranged within the support element 920, such that a secondportion 961B of the first busbar 961 and/or a second portion 962B of thesecond busbar 962 are/is exposed to the surface of the support element920 which is in contact with the first roller 901 and/or the secondroller 902. More specifically, the first busbar 961 and/or the secondbusbar 962 may be arranged within the support element 920 in analternating zig-zag pattern, as exemplary shown in FIG. 13 .

According to embodiments which can be combined with any otherembodiments described herein, the support element includes at least onematerial selected from the group consisting of: polytetrafluoroethylene(PTFE); fiber-reinforced polymer, particularly carbon-fiber-reinforcedpolymer; fiber-reinforced glass, polyamide and other suitable materials.Accordingly, beneficially the support element as described herein isconfigured for being flexible and providing a mechanical support for thefirst busbar and/or the second busbar and/or the flexible panels.

FIGS. 14A and 14B show a schematic top view of a flexible panel of thesupport element and a schematic back view of a flexible panel of thesupport element according to some embodiments described herein. Asexemplary shown in FIGS. 14A and 14B, according to embodiments which canbe combined with any other embodiments described herein, the at leastone conductive arrangement 960 may include a first electrode arrangement971 and/or a second electrode arrangement 972. In particular, the firstelectrode arrangement 971 and/or the second electrode arrangement 972may include multiple electrodes extending from a first side 940A of theflexible panel 940 towards an opposing second side 940B of the flexiblepanel 940, as exemplary shown in FIGS. 4A and 4B. For example, the firstelectrodes 971A of the first electrode arrangement 971 and the secondelectrodes 972A of the second electrode arrangement 972 may be arrangedin an alternating staggered manner. Accordingly, it is to be understoodthat the flexible panels 940 may be include neighboring electrodes whichcan be provided with opposite charge, as exemplarily indicated in FIGS.14A and 14B.

According to embodiments which can be combined with any otherembodiments described herein, the first electrodes 971A and the secondelectrodes 972A may be arranged parallel to each other. For example, thefirst electrodes 971A and the second electrodes 972A may be configuredas straight lines as exemplarily shown in FIGS. 14A and 14B.Alternatively, the first electrodes 971A and the second electrodes 972Amay have a different shape, for example the first electrodes 971A andthe second electrodes 972A can be configured to have a zig-zag pattern,a wavelike pattern, or the like.

According to embodiments which can be combined with any otherembodiments described herein, the first electrode arrangement 971 and/orthe second electrode arrangement 972 are provided within the at leastone flexible panel 940, as exemplarily shown in FIGS. 14A and 14B. Inparticular, the first electrode arrangement 971 and/or the secondelectrode arrangement 972 may be at least partially embedded in thematerial forming the flexible panel 940. For example, the flexible panel940 can be made of a flexible polymer such as polyamide.

More specifically, according to embodiments which can be combined withany other embodiments described herein, the top side of the flexiblepanel, i.e. the surface of the flexible panel which may contact the atleast one solar cell element when the at least one solar cell element issupported by the support element, is completely covered by the flexiblepolymer structure 942, e.g. a layer of polyamide. Typically, theflexible polymer structure 942 forms the main part of the flexiblepanel. Accordingly, it is to be understood that the electrodes ofdifferent polarity of the first electrode arrangement and the secondelectrode arrangement are integrated inside the flexible panel. Further,according to embodiments which can be combined with any other embodimentdescribed herein, the flexible panel 940, particularly opposingbacksides of the flexible panel, may include an adhesive portion 941configured for attaching the flexible panel 940 to the support element920. In particular, the adhesive portion 941 may be provided by two ormore adhesive portions which are arranged on opposing lateral edges ofthe flexible panel 940, as exemplarily shown in FIG. 14B. Typically, theadhesive portion 941 includes a portion of the first electrodearrangement 971 and/or the second electrode arrangement 972 which isconfigured for contacting the first busbar 961 and/or the second busbar962 when the flexible panel 940 is attached to the support element 920.

Accordingly, with exemplary reference to FIGS. 12, 14A and 14B, it is tobe understood that according to embodiments which can be combined withany other embodiments described herein, the at least one flexible panel940 can be releasable attached to the support element 920. Accordingly,beneficially a support device 900 for conveying at least one solar cellelement 910 is provided with modular and exchangeable flexible panelswhich are configured for providing an electrostatic force for holdingthe at least one solar cell element on the support element. Accordingly,beneficially embodiments of the support device as described hereinprovide for easy maintenance and replacement of flexible panels of thesupport device.

In FIG. 15 a detailed cross-sectional view of a layer structure of aflexible panel of the support element according to embodiments describedherein is shown. In particular, the flexible panel may include amultilayer structure having a bottom adhesive layer 943, a bottomsupporting layer 944, an intermediate adhesive layer 945 and a coverlayer 946, as exemplary shown in FIG. 15 . Typically, the firstelectrode arrangement 971 and/or the second electrode arrangement 972are/is arranged between bottom adhesive layer 943 and the cover layer946, more specifically between the bottom supporting layer 944 and theintermediate adhesive layer 945, as exemplarily indicated in FIG. 15 .

With exemplary reference to FIGS. 16 and 17 , according to embodimentswhich can be combined with any other embodiments described herein, thesupport element 920 may include two or more controllable regions whichcan be controlled with respects to the electrostatic force for holdingthe at least one solar cell element on the support element. Inparticular, the two or more controllable regions may for example beswitched between an “on”-state and an “off”-state. The “on”-state may bea state in in which an electrostatic force is generated and the“off”-state state may be a state in in which no electrostatic force isgenerated. Accordingly, beneficially a controllable support device canbe provided in which various regions of a support element canselectively be controlled in order to provide a local electrostaticforce for holding a sheet-like element, particularly a solar cellelement, on the support element.

According to embodiments which can be combined with any otherembodiments described herein, the support element 920 may include afirst controllable region Z1, a second controllable region Z2, a thirdcontrollable region Z3 and a fourth controllable region Z4, as exemplaryshown in FIG. 16 . In particular, the controllable regions may bearranged parallel to each other, particularly parallel to the transportdirection 911, as exemplary shown in FIG. 16 . Each of the controllableregions may include a first busbar 961 and a second busbar 962 asdescribed herein. Accordingly, each of the first busbars and the secondbusbars of the individual controllable regions Z1-Z4 may be suppliedwith an electrical charge as exemplarily described with reference toFIGS. 11 and 12 . Further, as exemplary shown for the first controllableregion Z1, at least one flexible panel 940 may be provided at the two ormore controllable regions.

With exemplary reference to FIG. 17 , according to embodiments which canbe combined with any other embodiments described herein, the supportelement 920 may be configured such that individual flexible panels canbe controlled separately from each other. In particular, the individualflexible panels may be controlled such that the flexible panels can beswitched from an “on”-state in which an electrostatic force is generatedto an “off”-state in which no electrostatic force is present.Accordingly, the support element 920 can be configured such that two ormore flexible panels as described herein can be provided with anelectrical charge. For example, the support element 920 may include fourfirst busbars 961A-961D and four second busbars 962A-962D, which arearranged such that for example four flexible panels Z1-Z4 as describedherein can individually be provided with an electrical charge separatelyfrom each other.

In view of the embodiments of the electrostatic support device asdescribed in the present disclosure, it is to be understood thatembodiments of the electrostatic support device are particularly wellsuited for holding thin sheet-like elements, e.g. solar cell elements,particularly photovoltaic panel elements, using electrostatic attractiveforces between the thin sheet like elements and the supportelectrostatic device. For example, the electrostatic support device maybeneficially be used for holding and conveying photovoltaic panelelements during production, e.g. during drying or serigraphic processes.More specifically, the electrostatic support device may in particular bebeneficial to transport thin sheet-like elements by employing aconveying belt moving in a continuous mode in order to transport thinsheet-like elements between different processing stations. Further,providing a support element including modular flexible panels asdescribed herein allows for easy maintenance and replacement procedures.

Further, according to embodiments which can be combined with any otherembodiments described herein, a method for conveying at least one solarcell element in a transport direction is provided. In particular, themethod includes providing an electric charge to a support elementconfigured for supporting at least one solar cell element; holding theat least one solar element by an electrostatic force; and moving the atleast one solar element in a transport direction.

For example, providing an electric charge to a support element mayinclude employing a support element according to embodiments describedherein. Accordingly, holding the at least one solar element by anelectrostatic force may include using an electric arrangement asdescribed herein. Accordingly, it is to be understood that the methodfor conveying at least one solar cell element may be conducted byemploying a support device as described herein.

According to embodiments which can be combined with any otherembodiments described herein, a support device 900 for conveying atleast one solar cell element 910 in a transport direction 911 isprovided. The support device includes a support element 920 configuredfor supporting the at least one solar cell element and an electricarrangement 950 configured for providing an electrostatic force forholding the at least one solar cell element on the support element.

According to embodiments which can be combined with any otherembodiments described herein, the electric arrangement 950 includes acharging source 951 configured for providing an electrostatic charge tothe support element 920.

According to embodiments which can be combined with any otherembodiments described herein, the electric arrangement 950 includes atleast one conductive arrangement 960 configured for receiving anelectrostatic charge from the charging source 951.

According to embodiments which can be combined with any otherembodiments described herein, the at least one conductive arrangement960 is configured for providing the electrostatic force for holding theat least one solar cell element 910 on the support element 920.

According to embodiments which can be combined with any otherembodiments described herein, the at least one conductive arrangement960 includes a first busbar 961 and/or a second busbar 962.

According to embodiments which can be combined with any otherembodiments described herein, the at least one conductive arrangement960 includes a first electrode arrangement 971 and/or a second electrodearrangement 972.

According to embodiments which can be combined with any otherembodiments described herein, the first electrode arrangement 971 and/orthe second electrode arrangement 972 are provided within at least oneflexible panel 940.

According to embodiments which can be combined with any otherembodiments described herein, the flexible panel 940 is releasableattached to the support element 920.

According to embodiments which can be combined with any otherembodiments described herein, the flexible panel 940 includes anadhesive portion 941 configured for attaching the flexible panel to thesupport element 920.

According to embodiments which can be combined with any otherembodiments described herein, the support device 900 further includes atleast a first roller 901 and a second roller 902 configured for movingthe support element 920 in the transport direction 911.

According to embodiments which can be combined with any otherembodiments described herein, the electric arrangement 950 includes anelectrical grounding for grounding the support element 920.

According to embodiments which can be combined with any otherembodiments described herein, the electrical grounding is provided by atleast one roller of the first roller 901 and the second roller 902.

According to embodiments which can be combined with any otherembodiments described herein, the electrical grounding is provided by agrounding roller 903 configured for grounding the support element.

According to embodiments which can be combined with any otherembodiments described herein, the support element is a belt conveyor.

According to embodiments which can be combined with any otherembodiments described herein, the support element includes at least onematerial selected from the group consisting of: polytetrafluoroethylene(PTFE); fiber-reinforced polymer, particularly carbon-fiber-reinforcedpolymer; fiber-reinforced glass, polyamide and other suitable materials.

According to embodiments which can be combined with any otherembodiments described herein, a method for conveying at least one solarcell element 910 in a transport direction 911 is provided. The methodincludes providing an electric charge to a support element configuredfor supporting at least one solar cell element; holding the at least onesolar element by an electrostatic force; and moving the at least onesolar element in a transport direction.

The embodiments of the present disclosure separate, e.g., cleaves asolar cell into smaller pieces, which are then allocated to at least twodifferent solar cell arrangements. As an example, each piece can beallocated to a respective solar cell arrangement based on one or moregeometric and/or physical properties of the piece. A solar cellarrangement can thus be made of solar cell elements having similarcharacteristics and/or quality, and an overall efficiency of the solarcell arrangement can be improved. A module power office solar cellmodule having the solar cell arrangement can be increased, particularlysince the occurrence of “bottlenecks” can be avoided.

According to one aspect of the present disclosure, an apparatus formanufacture of at least two solar cell arrangements is provided. Theapparatus includes: a separation device configured for separating afirst solar cell into two or more first solar cell pieces; and at leastone positioning device configured for positioning at least one firstsolar cell piece of the two or more first solar cell pieces on a supportdevice for forming a first solar cell arrangement of the at least twosolar cell arrangements and for positioning at least one other firstsolar cell piece of the two or more first solar cell pieces on thesupport device for forming a second solar cell arrangement of the atleast two solar cell arrangements.

According to embodiments which can be combined with other embodimentsdescribed herein, the at least one positioning device is configured toarrange a plurality of solar cell pieces including the at least onefirst solar cell piece on the support device with adjacent solar cellpieces partly overlapping with each other to form the first solar cellarrangement, and is configured to arrange a plurality of other solarcell pieces including the at least one other first solar cell piece onthe support device with adjacent solar cell pieces partly overlappingwith each other to form the second solar cell arrangement.

According to embodiments which can be combined with other embodimentsdescribed herein, the separation device is configured for separating asecond solar cell into two or more second solar cell pieces, wherein thepositioning device is configured for positioning at least one secondsolar cell piece of the one or more second solar cell pieces on thesupport device for forming the first solar cell arrangement togetherwith the at least one first solar cell piece, and is configured forpositioning at least one other second solar cell piece of the two ormore second solar cell pieces on the support device for forming thesecond solar cell arrangement together with the at least one other firstsolar cell piece.

According to embodiments which can be combined with other embodimentsdescribed herein, the separation device is configured for sequentiallyor simultaneously separating the first solar cell and the second solarcell into the two or more first solar cell pieces and the two or moresecond solar cell pieces, respectively.

According to embodiments which can be combined with other embodimentsdescribed herein, the separation device includes a first cleaving deviceconfigured for separating the first solar cell into the two or morefirst solar cell pieces and a second cleaving device configured forseparating the second solar cell into the two or more second solar cellpieces.

According to embodiments which can be combined with other embodimentsdescribed herein, the separation device includes at least one solar cellperforation device.

According to embodiments which can be combined with other embodimentsdescribed herein, the at least one solar cell perforation deviceincludes a laser.

According to embodiments which can be combined with other embodimentsdescribed herein, the apparatus is configured to allocate each solarcell piece of the two or more first solar cell pieces to either thefirst solar cell arrangement or the second solar cell arrangement basedon one or more properties of the respective solar cell piece of the twomore first solar cell pieces.

According to embodiments which can be combined with other embodimentsdescribed herein, the apparatus further includes at least one of a firstinspection device, a second inspection device, and a third inspectiondevice, wherein the first inspection device is configured to measureand/or determine one or more properties of the first solar cell beforethe solar cell is separated into the two or more first solar cellpieces, wherein the second inspection device is configured to measureand/or determine one or more properties of the two or more first solarcell pieces of the first solar cell after the solar cell has beenseparated into the two or more first solar cell pieces, and wherein thethird inspection device is configured to measure and/or determine one ormore properties of the first solar cell arrangement and/or the secondsolar cell arrangement.

According to embodiments which can be combined with other embodimentsdescribed herein, the one or more properties are selected from the groupconsisting of geometric shape, electrical properties, opticalproperties, printing quality, and any combination thereof.

According to embodiments which can be combined with other embodimentsdescribed herein, the support device includes at least one of anelectrostatic chuck and a vacuum chuck.

According to embodiments which can be combined with other embodimentsdescribed herein, the support device includes at least a belt conveyor,wherein the at least a belt conveyor is configured to support, fix andtransport the first solar cell arrangement and the second solar cellarrangement.

According to embodiments which can be combined with other embodimentsdescribed herein, a movement of the belt conveyor and a movement of theat least one positioning device are synchronized with each other.

According to embodiments which can be combined with other embodimentsdescribed herein, the at least a belt conveyor includes a first beltconveyor configured to support the first solar cell arrangement and asecond belt conveyor spaced apart from the first belt conveyor andconfigured to support the second solar cell arrangement.

According to embodiments which can be combined with other embodimentsdescribed herein, the apparatus further includes a heating device at thesupport device, wherein the heating device is configured to heat atleast one of the first solar cell arrangement and the second solar cellarrangement.

According to embodiments which can be combined with other embodimentsdescribed herein, the apparatus further includes an adhesive applicationdevice configured to apply an adhesive to the first solar cell or thetwo or more first pieces before the two or more first pieces arepositioned on the support device.

According to embodiments which can be combined with other embodimentsdescribed herein, the apparatus further includes a sorting deviceconfigured for sorting the first solar cell arrangement and the secondsolar cell arrangement based to a quality determination of the firstsolar cell arrangement and the second solar cell arrangement.

According to embodiments which can be combined with other embodimentsdescribed herein, the at least one positioning device includes vacuumgrippers for gripping the two or more first solar cell pieces.

According to another aspect of the present disclosure, a system formanufacture of at least two shingled solar cells is provided. The systemcomprising the apparatus according to any one of the embodimentsdescribed herein and a production tool for manufacturing a plurality ofsolar cells including the first solar cell, wherein the plurality ofsolar cells are input into the apparatus.

According to embodiments which can be combined with other embodimentsdescribed herein, the production tool includes one or more printingdevices configured for printing one or more conductive lines on solarcell substrates used in the manufacture of the plurality of solar cells,wherein the one or more conductive lines are selected from fingers andbusbars.

According to embodiments which can be combined with other embodimentsdescribed herein, the one or more printing devices are configured fordouble printing of at least one of the fingers and busbars.

According to a further aspect of the present disclosure, a method formanufacture of at least two solar cell arrangements is provided. Themethod comprising: separating each solar cell of one or more solar cellsinto two or more solar cell pieces; and forming at least a first solarcell arrangement and a second solar cell arrangement of the at least twosolar cell arrangements from the two or more solar cell pieces, whereineach solar cell piece of the two or more solar cell pieces is allocatedto the first solar cell arrangement or the second solar cell arrangementbased on one or more geometric and/or physical properties of the solarcell piece.

According to embodiments which can be combined with other embodimentsdescribed herein, the one or more geometric and/or physical propertiesare selected from the group consisting of geometric shape, electricalproperties, optical properties, and any combination thereof.

According to embodiments which can be combined with other embodimentsdescribed herein, the method further includes determining the one ormore geometric and/or physical properties at least one of before theseparating of each solar cell and after the forming of the first solarcell arrangement and the second solar cell arrangement.

According to embodiments which can be combined with other embodimentsdescribed herein, each solar cell of the one or more solar cells isseparated into two, three, four, five, six, or more solar cell pieces.

According to embodiments which can be combined with other embodimentsdescribed herein, the one or more solar cells are selected from thegroup consisting of full-square solar cells and pseudo-square solarcells.

According to embodiments which can be combined with other embodimentsdescribed herein, the method further includes gripping the two or moresolar cell pieces; and positioning the two or more solar cell pieces ona support device to form the first solar cell arrangement and the secondsolar cell arrangement.

According to embodiments which can be combined with other embodimentsdescribed herein, the method further includes applying an adhesive tothe two or more solar cell pieces before positioning the two or moresolar cell pieces on the support device.

According to embodiments which can be combined with other embodimentsdescribed herein, the method further includes drying the adhesive whilethe two or more solar cell pieces are fixed to the support device.

According to embodiments which can be combined with other embodimentsdescribed herein, solar cell pieces of the two or more solar cell piecescorresponding to a predetermined geometric shape are allocated to eitherthe first solar cell arrangement or the second solar cell arrangement.

While the foregoing is directed to embodiments of the disclosure, otherand further embodiments of the disclosure may be devised withoutdeparting from the basic scope thereof, and the scope thereof isdetermined by the claims that follow.

The invention claimed is:
 1. Method for manufacture of a plurality ofsolar cell arrangements, the method comprising: separating a first solarcell into two or more first solar cell pieces; separating a second solarcell into two or more second solar cell pieces; positioning at least oneof the two or more first solar cell pieces on a support device forforming a first solar cell arrangement; positioning at least one of thetwo or more second solar cell pieces on the support device for forming asecond solar cell arrangement; and positioning at least one other of thetwo or more first solar cell pieces and at least one other of the two ormore second solar cell pieces on the support device for forming a thirdsolar cell arrangement.
 2. The method of claim 1, wherein the firstsolar cell is separated by a first cleaving device and the second solarcell is separated by a second cleaving device.
 3. The method of claim 1,further comprising: assembling the first solar cell arrangement, thesecond solar cell arrangement and the third solar cell arrangement inparallel to each other on the support device.
 4. The method of claim 1,wherein the at least one first solar cell piece and the at least onesecond solar cell piece are full-square pieces, and the at least oneother first solar cell piece and the at least one other second solarcell piece are pseudo-square pieces.
 5. The method of claim 1, whereinthe first solar cell and the second solar cell are separated by at leastone separation device, the method further comprising: moving the atleast one first solar cell piece from the at least one separation deviceonto a first transportation lane; moving the at least one second solarcell piece from the at least one separation device onto a secondtransportation lane; and moving laterally the at least one other firstsolar cell piece and the at least one other second solar cell piece fromthe at least one separation device onto a third transportation lane. 6.The method of claim 5, wherein the first, second and thirdtransportation lanes are belt conveyors spaced apart from each other. 7.The method of claim 1, wherein the support device comprises at least abelt conveyor, the method further comprising: supporting, fixing and/ortransporting the first solar cell arrangement, the second solar cellarrangement and the third solar cell arrangement by the at least a beltconveyor.
 8. The method of claim 7, wherein the at least a belt conveyorcomprises a first belt conveyor, a second belt conveyor spaced apartfrom the first belt conveyor and a third belt conveyor spaced apart fromthe first and second belt conveyors, the method further comprising:supporting the first solar cell arrangement by the first belt conveyor;supporting the second solar cell arrangement by the second beltconveyor; and supporting the third solar cell arrangement by the thirdbelt conveyor.
 9. The method of claim 7, wherein the at least one firstsolar cell piece, the at least one second solar cell piece, the at leastone other first solar cell piece and the at least one other second solarcell piece are positioned on the support device by at least onepositioning device, wherein a movement of the at least a belt conveyorand a movement of the at least one positioning device are synchronizedwith each other.
 10. The method of claim 1, wherein the third solar cellarrangement is positioned between the first solar cell arrangement andthe second solar cell arrangement.
 11. The method of claim 1, furthercomprising at least one of: measuring and/or determining one or moreproperties of the first solar cell and the second solar cell before thefirst solar cell is separated into the two or more first solar cellpieces and the second solar cell is separated into the two or moresecond solar cell pieces; measuring and/or determining one or moreproperties of the two or more first solar cell pieces of the first solarcell and the two or more second solar cell pieces of the second solarcell after the first solar cell has been separated into the two or morefirst solar cell pieces and the second solar cell has been separatedinto the two or more second solar cell pieces; and measuring and/ordetermining one or more properties of the first solar cell arrangement,the second solar cell arrangement and/or the third solar cellarrangement.
 12. The method of claim 1, further comprising: arranging aplurality of solar cell pieces including the at least one first solarcell piece on the support device with adjacent solar cell pieces partlyoverlapping with each other to form the first solar cell arrangement;arranging a plurality of other solar cell pieces including the at leastone second solar cell piece on the support device with adjacent solarcell pieces partly overlapping with each other to form the second solarcell arrangement; and arranging the at least one other first solar cellpiece and the at least one other second solar cell piece on the supportdevice with adjacent solar cell pieces partly overlapping with eachother to form the third solar cell arrangement.
 13. Method formanufacture of a plurality of solar cell arrangements, the methodcomprising: positioning at least one first solar cell piece of a firstsolar cell for forming a first solar cell arrangement; positioning atleast one second solar cell piece of a second solar cell for forming asecond solar cell arrangement; positioning at least one other firstsolar cell piece of the first solar cell and at least one other secondsolar cell piece of the second solar cell for forming a third solar cellarrangement; and supporting the first solar cell arrangement, the secondsolar cell arrangement and the third solar cell arrangement by a supportdevice.
 14. Method for manufacture of at least two solar cellarrangements, comprising: separating a first solar cell into at leastone first pseudo-square solar cell piece and at least one firstfull-square solar cell piece; separating a second solar cell into atleast one second pseudo-square solar cell piece and at least one secondfull-square solar cell piece; positioning one or more of the at leastone first pseudo-square solar cell piece and one or more of the at leastone second pseudo-square solar cell piece on a belt conveyor for forminga first solar cell arrangement of the at least two solar cellarrangements; and positioning one or more of the at least one firstfull-square solar cell piece and one or more of the at least one secondfull-square solar cell piece on the belt conveyor for forming a secondsolar cell arrangement of the at least two solar cell arrangements, sothat the first solar cell arrangement and the second solar cellarrangement are supported by the same belt conveyor.
 15. The method ofclaim 14, further comprising: assembling the first solar cellarrangement and the second solar cell arrangement in parallel to eachother on the support device.
 16. The method of claim 14, furthercomprising: arranging the at least one first solar cell piece and the atleast one second solar cell piece on the support device with adjacentsolar cell pieces partly overlapping with each other to form the firstsolar cell arrangement; and arranging the at least one other first solarcell piece and the at least one other second solar cell piece on thesupport device with adjacent solar cell pieces partly overlapping witheach other to form the second solar cell arrangement.
 17. The method ofclaim 14, wherein the first solar cell is separated into the at leastone first solar cell piece and the at least one other first solar cellpiece using a first cleaving device, and the second solar cell isseparated into the at least one second solar cell piece and the at leastone other second solar cell piece using a second cleaving device. 18.The method of claim 14, further including at least one of: measuringand/or determining one or more properties of the first solar cell andthe second solar cell before the first solar cell is separated into theat least one first solar cell piece and the at least one other firstsolar cell piece and the second solar cell is separated into the atleast one second solar cell piece and at least one other second solarcell piece; measuring and/or determining one or more properties of theat least one first solar cell piece and the at least one other firstsolar cell piece of the first solar cell after the first solar cell hasbeen separated into the at least one first solar cell piece and the atleast one other first solar cell piece, and one or more properties ofthe at least one second solar cell piece and the at least one othersecond solar cell piece of the second solar cell after the second solarcell has been separated into the at least one second solar cell pieceand at least one other second solar cell piece; and measuring and/ordetermining one or more properties of the first solar cell arrangementand/or the second solar cell arrangement.
 19. The method of claim 14,wherein the support device includes at least a belt conveyor, the methodfurther comprising: supporting, fixing and/or transporting the firstsolar cell arrangement and the second solar cell arrangement by the atleast a belt conveyor.
 20. The method of claim 19, wherein the one ormore of the at least one first solar cell piece, the one or more of theat least one second solar cell piece, the one or more of the at leastone other first solar cell piece and the one or more of the at least oneother second solar cell piece are positioned on the support device usingat least one positioning device, wherein a movement of the at least abelt conveyor and a movement of the at least one positioning device aresynchronized with each other.
 21. The method of claim 19, wherein the atleast a belt conveyor includes a first belt conveyor and a second beltconveyor spaced apart from the first belt conveyor, the method furthercomprising: supporting the first solar cell arrangement by the firstbelt conveyor; and supporting the second solar cell arrangement by thesecond belt conveyor.
 22. Method for manufacture of at least two solarcell arrangements, comprising: separating a first solar cell into two ormore first solar cell pieces by a separation device; separating a secondsolar cell into two or more second solar cell pieces by the separationdevice, wherein the first solar cell and the second solar cell aresequentially separated by the separation device into the two or morefirst solar cell pieces and the two or more second solar cell pieces,respectively; positioning the two or more first solar cell pieces on asupport device for forming a first solar cell arrangement of the atleast two solar cell arrangements; positioning the two or more secondsolar cell pieces on the support device for forming a second solar cellarrangement of the at least two solar cell arrangements; and assemblingthe first solar cell arrangement and the second solar cell arrangementin parallel to each other on the support device.
 23. The method of claim22, further comprising: arranging the two or more first solar cellpieces on the support device with adjacent solar cell pieces partlyoverlapping with each other to form the first solar cell arrangement;and arranging the two or more second solar cell pieces on the supportdevice with adjacent solar cell pieces partly overlapping with eachother to form the second solar cell arrangement.
 24. The method of claim22, further comprising: separating a third solar cell into two or morethird solar cell pieces; separating a fourth solar cell into two or morefourth solar cell pieces; positioning the two or more third solar cellpieces on the support device for forming the first solar cellarrangement together with the two or more first solar cell pieces; andpositioning the two or more fourth solar cell pieces on the supportdevice for forming the second solar cell arrangement together with thetwo or more second solar cell pieces.
 25. The method of claim 22,wherein the first solar cell is separated into the two or more firstsolar cell pieces using a first cleaving device and the second solarcell is separated into the two or more second solar cell pieces using asecond cleaving device.
 26. The method of claim 22, further including atleast one of: measuring and/or determining one or more properties of thefirst solar cell and the second solar cell before the first solar cellis separated into the two or more first solar cell pieces and the secondsolar cell is separated into the two or more second solar cell pieces;measuring and/or determining one or more properties of the two or morefirst solar cell pieces of the first solar cell and the two or moresecond solar cell pieces of the second solar cell after the first solarcell has been separated into the two or more first solar cell pieces,and the second solar cell has been separated into the two or more secondsolar cell pieces; and measuring and/or determining one or moreproperties of the first solar cell arrangement and/or the second solarcell arrangement.
 27. The method of claim 22, wherein the support deviceincludes at least a belt conveyor, the method further comprising:supporting, fixing and/or transporting the first solar cell arrangementand the second solar cell arrangement by the at least a belt conveyor.28. The method of claim 27, wherein the two or more first solar cellpieces and the two or more second solar cell pieces are positioned onthe support device using at least one positioning device, wherein amovement of the belt conveyor and a movement of the at least onepositioning device are synchronized with each other.
 29. The method ofclaim 27, wherein the at least a belt conveyor includes a first beltconveyor and a second belt conveyor spaced apart from the first beltconveyor, the method further comprising: supporting the first solar cellarrangement by the first belt conveyor; and supporting the second solarcell arrangement by the second belt conveyor.